N465AW

Part: ANTI-ICE VALVE — FAULTED (RH ENGINE) · airframe 41,793 hrs · 40,806 cycles

INFIGHTING REC'D "R COWL A/I" CAUTION WITH SWITCH SELECTED OFF. FOUND R COWL PRV POPPED ON POST FLIGHT. AIRCRAFT REMOVED FROM SERVICE R&R RH COWL PRESSURE RELIEF VALVE REF 30-2204. OPS CHECK GOOD

Part: SENSOR — FAULTED (WS291.5) · airframe 41,107 hrs · 40,453 cycles

UPON DEPARTURE AND CLIMB OUT OF KDAY FLAP FAILED WITH INDICATION OF 0. CREW HAS ELECTED TO FLY ONTO KORD. CREW HAS DECLARED AN EMERGENCY FOR FLAP FAILURE. CREW IS SCHEDULED TO ARRIVE AT KORD AT 0838 CENTRAL TIME. AIRCRAFT REMOVED FROM SERVICE. R&R L BPSU IAW AMM 27-51-10 UP TO AND INCLUDING FLAP RIG. REF LP 353430-1 FOR FLEX SHAFT SAFETY AND PANEL INSTALLATION AND OPS CHECK DUE.

Part: FCU — FAULTED (TE FLAPS) · airframe 41,048 hrs · 39,959 cycles

RECEIVED FLAP FAIL MESSAGE BEFORE DESCENT. AIRCRAFT REMOVED FROM SERVICE. T/S PER FIM 27-50 FIG 108, FECU #1 MOST PROBABLE FAULT #12 PRESENT. REPLACED THE FECU PER AMM 27-51-05, OPS CHECK GOOD. REMOVED PLACARD/MEL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,489 hrs · 39,333 cycles

GEAR DISAGREE ON TAKE-OFF. WARNING MESSAGE APPEARED WITHIN 5 SECS OF SELECTION. NLG DID NOT MOVE. MLG RETRACTED NORMALLY. NOSE DOOR OPEN MESSAGE ALSO APPEARED. C/W QRH. RECEIVED THREE GREEN DOWN AND LOCKED. LANDING AT 46,500 LBS. BELOW LANDING WEIGHT. AIRCRAFT REMOVED FROM SERVICE. R & R NLG PROX SENSOR BRACKET. OPS CHECK GOOD.

Part: STIFFENER — MISSING (BS 621 BULKHEAD) · airframe 39,454 hrs · 38,132 cycles

AFT PRESSURE BULKHEAD FS621 IS MISSING ALL REINFORCEMENT ANGLES, AIRCRAFT REMOVED FROM SERVICE. INSTALLED REINFORCEMENT ANGLES TO AFT PRESSURE BULKHEAD FS621. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-53-61-1240 REV (D).

Part: DRAG ANGLE — CRACKED (BS 310 - 349) · airframe 39,454 hrs · 38,132 cycles

PAX DOOR AFT PANEL DRAG ANGLE IS CRACKED AT PULLEY BRACKET AREA. AIRCRAFT REMOVED FROM SERVICE. REPAIRED DRAG ANGLE. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-52-11-513 REV C.

Part: ANGLE — CORRODED (BS 310, RBL 43) · corrosion level 2 · airframe 39,454 hrs · 38,132 cycles

CORROSION ON SERVICE DOOR LOWER SILL ANGLE P/N 601R38303-253 AT FS 310.0 AND RBL 43. AIRCRAFT REMOVED FROM SERVICE. REMOVED DAMAGE BY BLENDING SERVICE DOOR LOWER SILL ANGLE AT FS310.0 AND RBL 43. ORIGINAL MATERIAL THICKNESS 0.063. REMAINING THICKNESS 0.050 PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW EA AWAC-CRJ253-01941 REV A,

Part: SKIN — CORRODED (RH IB FLAP) · corrosion level 2 · airframe 39,454 hrs · 38,132 cycles

RIGHT HAND WING INBOARD FLAP INBOARD SIDE LOWER SKIN PN 601R4008 HAS CORROSION AND 5 GOUGES AT INBOARD WING STATION 50.498 - 79.062. ***********AIRCRAFT REMOVED FROM SERVICE**************** BLENDED OUT CORROSION IAW CRJ200 SRM 51-12-00 REV 39 AND SRM 51-21-06 REV 39. BLENDED GOUGE DAMAGES TO A SMOOTH CONTOUR. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW EA #: AWAC-CRJ257 - 01935 REV IR, DATED 12/19/2022. WORK PERFORMED UNDER AERSALE WORK ORDER 003813, CARD NO. 20079, TT: 39,454:52 TC: 38132.

Part: FLOORBEAM — CRACKED (BS 621 LBL27-43) · corrosion level 2 · airframe 39,454 hrs · 38,132 cycles

CORROSION AND CRACK ON CABIN FLOORBEAM AT BS 621, LBL 27-43. AIRCRAFT REMOVED FROM SERVICE. BLENDED CORROSION, REMOVED AND REPLACED THE SECTION OF ANGLE. HFEC PERFORMED WITH NO INDICATIONS IAW NDT 51-20-06 REV 44 PART 1. RESTORED SURFACE FINISH. WORK WITHIN LIMITS WAS PERFORMED IAW SRM 53-00-00, REV 39, SRM 51-21-06, REV 39, SRM 53-61-43, REV 39, SRM 51-11-00, REV 39, SRM 51-21-11, REV 39, AND SRM 51-40-11. REV 39.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 39,454 hrs · 38,132 cycles

CORROSION ON FLOOR STRUCTURE RH STRAP, BS 559, RBL 27 - 42. REMOVED AND INSTALLED FLOOR STRUCTURE RT STRAP WITH FABRICATED STRAP . RESTORED SURFACE FINISH. PERFORMED IAW 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.

Part: RIB — DAMAGED (RT WING) · airframe 39,454 hrs · 38,132 cycles

RIGHT WINGLET ATTACH STRUCTURE HAS ONE ELONGATED HOLE ON RIB AND STRAP AT WS404.08. REPAIRED THE RT WINGLET ATTACH STRUCTURE BY REPLACING STRAP, INSTALLED FREEZE PLUG AND COUNTERBORED FREEZE PLUG. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-57-31-1410 REV -.

Part: FLOORBEAM — CORRODED (BS 349 RBL 28-42) · corrosion level 2 · airframe 39,454 hrs · 38,132 cycles

CORROSION ON CABIN FLOOR STRUCTURE SUPPORT ANGLE AT SERVICE DOOR FS349 AND RBL28 TO RBL42. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ANGLE SUPPORT ANGLE AT SERVICE DOOR FS349 AND RBL28 TO RBL42. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW SRM 53-21-15 REV 39, SRM 53-00-00 REV 39, SRM 51-42-06 REV 39, SRM 51-42-20 REV 39.

Part: SEAT TRACK — CORRODED (BS 559 -559 + 84) · corrosion level 2 · airframe 39,454 hrs · 38,132 cycles

CORROSION ON RT SEAT TRACK FROM BS 559 - 559+84, RBL 9. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION, PERFORMED HFEC WITH NO INDICATIONS IAW NDTM 51-20-06 PART 1, REV 44. RESTORED PROTECTIVE FINISH. WORK WITHIN LIMITS IAW AMM 53-01-11 REV 66, REPLACED THE SEAT TRACK IAW SRM 53-41-49 REV 39, SRM 53-31-49 REV 39, SRM 53-21-49 REV 39, SRM 53-51-49 REV 39, SRM 53-41-02 REV 39, SRM 53-40-11 REV 39, SRM 51-21-11 REV 39, SRM 51-26-00 REV 39, SRM 51-21-06 REV 39, SRM 51-25-06 REV 39 AND SRM 51-25-116 REV 39.

Part: RIB — DAMAGED (LT WING) · airframe 39,454 hrs · 38,132 cycles

LH WINGLET ATTACH STRUCTURE HAS ONE ELONGATED HOLE ON RIB AT WS404.08. REPAIRED LH WINGLET ATTACH STRUCTURE BY REPLACING RIB P AT WS404.08 AND WGLT3.25. INSTALLED FREEZE PLUG AND COUNTERBORED FREEZE PLUG. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-57-31-1411 REV-.

Part: FLOORBEAM — CORRODED (BS 349 RBL 19-21) · corrosion level 2 · airframe 39,454 hrs · 38,132 cycles

CORROSION ON CABIN FLOOR STRUCTURE SUPPORT P/N 601R38672-1 AT FS349.0 AND RBL19.0 TO RBL21. REMOVED CORROSION BY BLENDING CABIN FLOOR STRUCTURE SUPPORT. PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW ASAP EA CRJ253-01940 REV A,

Part: SKIN — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 39,454 hrs · 38,132 cycles

CORROSION ON LEFT WING INBOARD FLAP LOWER SKIN FROM WS50.498- WS100.009. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DAMAGED SECTION ON LEFT WING INBOARD FLAP LOWER SKIN FROM WS50.498 WS100.009. CUTOUT DIMENSIONS L= 29.700X W= 21.250. RESTORED SURFACE PROTECTIVE FINISH. PERFORMED HFEC WITH NO INDICATIONS. ALL WORK WITHIN LIMITS PERFORMED IAW EA AWAC-CRJ257-01943 REV IR,

Part: FLOORBEAM — CORRODED (BS 349) · corrosion level 2 · airframe 39,454 hrs · 38,132 cycles

CORROSION ON CABIN FLOOR STRUCTURE CROSSBEAM AT FS349.0 AND RBL19.0 TO RBL24. REMOVED CORROSION BY BLENDING CABIN FLOOR STRUCTURE CROSSBEAM P/N 601R32005-149 AT FS349.0 AND RBL19.0 TO RBL24. FABRICATED STRAP FROM 0.050Ï¿½ ALUM. SHEET MATERIAL HEAT TREATED TO 7075-T6. STRAP DIMENSIONS L= 7.50Ï¿½ X W= 0.080Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE PROTECTIVE FINISH. ALL WORK WITHIN LIMITS PERFORMED IAW ASAP EA #: AWAC-CRJ253-01938 REV IR,

Part: FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 39,454 hrs · 38,132 cycles

CORROSION ON PAX DOOR FWD ANCHOR FITTING AT BS 310, WL 75. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ON PAX DOOR FWD ANCHOR FITTING. RESTORED PROTECTIVE FINISH. WORK WITHIN LIMITS, PERFORMED IAW AMM 52-11-17-400-804, REV 66, ADJUSTMENT IAW AMM 52-11-17-820-802, REV 66.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 39,454 hrs · 38,132 cycles

CORROSION ON PAX DOOR AFT ANCHOR FITTING, PLATE AND COVER AT BS 349, WL 75. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED PAX DOOR AFT ANCHOR FITTING, PLATE, AND COVER. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AMM 52-11-17-400-804, REV 66, ADJUSTMENT IAW AMM 52-11-17-820-802, REV 66.

Part: HOUSING — LEAKING (SCAV OIL FILTER) · airframe 37,105 hrs · 35,818 cycles

AT 3,000-3,500 FEET RH ENGINE OIL (PSI) FLUXUATION FROM 15 PSI TO 51 PSI, EVEN AT CRUISING POWER, C/W QRH, AIR RETURN. AIRCRAFT REMOVED FROM SERVICE. UPON FURTHER INSPECTION FOUND OIL TO BE LEAKING FROM SCAVENGER OIL FILTER HOUSING. FOUND OIL FILTER HOUSING CAP TO BE MISSING AN ORING. INSTALLED ORING IN REF AMM 79-21-05. NO LEAKS NOTED. NO DEFECTS AT THIS TIME. A/C PLACED ON DAILY OIL WATCH FOR LH ENGINE. DUE TO TAKING 10 PINTS OF OIL.

Part: ANGLE — CRACKED (FS318) · airframe 37,073 hrs · 35,778 cycles

CRACKED ANGLE ON PASSENGER DOOR FORWARD SIDE WALL PANEL AT 2ND STEP. FS318 PAX DOOR P/N 601R31701-1 S/N 7896 ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED PASSENGER DOOR FORWARD SIDE PANEL ANGLE P/N 601R-52-11-702-10 WITH FABRICATED ANGLE, FS318. RESTORED SURFACE FINISH. ALL WORK PERFORMED IAW REO 601R-52-11-702 REV E, DATED 2016-08-14.

Part: ANGLE — CRACKED (FS 340) · airframe 37,073 hrs · 35,778 cycles

TWO CRACKED ANGLES ON PASSENGER DOOR AFT SIDE WALL PANEL AT 2ND STEP. FS340. PAX DOOR P/N 601R31701-1 S/N 7896 ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED PASSENGER DOOR FORWARD SIDE PANEL ANGLES P/N 601R-52-11-702-7 AND 601R-52-11-702-9 WITH FABRICATED ANGLE, FS340. RESTORED SURFACE FINISH. ALL WORK PERFORMED IAW REO 601R-52-11-702 REV E, DATED 2016-08-14.

Part: STRAP — GOUGED (LT WINGLET) · airframe 37,073 hrs · 35,778 cycles

LH WINGLET HAS 3 GOUGES AT INBOARD AND OUTBOARD LOWER FORWARD STRAPS, WS389. P/N 600-15108-7 AND P/N 600-15108-18. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED 2 GOUGES AT LH LOWER FORWARD WINGLET OUTBOARD STRAP P/N 600-15108-7. DIMENSIONS 3.200Ï¿½L X 2.00Ï¿½W. PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW ASAP EA # AWAC-CRJ257-01637 REV A DATED 5/25/2021. BLENDED 1 GOUGE AT LH LOWER FORWARD WINGLET INBOARD STRAP P/N 600-15108-18. DIMENSIONS 1.600Ï¿½L X 0.400Ï¿½W. PERFORMED HFEC WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK WITHIN LIMITS AND PERFORMED IAW ASAP EA # AWAC-CRJ257-01638 REV A DATED 5/25/2021.

Part: ANGLE — CRACKED (FS 318) · airframe 37,073 hrs · 35,778 cycles

CRACKED ANGLE ON PASSENGER DOOR FORWARD LOWER SIDE WALL PANEL AT LOWER STEP. FS318 PAX DOOR P/N 601R31701-1 S/N 7896 ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED PASSENGER DOOR FORWARD LOWER SIDE WALL PANEL AT LOWER STEP, ANGLE P/N 601R-52-11-702-44, SHIM P/N 601R-52-11-702-43 AND TAPERED SHIM P/N 601R52-11-702-45 WITH FABRICATED PARTS, FS318. RESTORED SURFACE FINISH. PERFORMED HFEC WITH NO INDICATIONS. ALL WORK PERFORMED IAW REO 601R-52-11-702 REV E, DATED 2016-08-14

Part: SKIN — GOUGED (FS 589) · airframe 37,073 hrs · 35,778 cycles

AFT FUSELAGE SKIN GOUGE FS 589.00 + 1Ï¿½ RH STR 25 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN GOUGE FS 589.00 + 1 RH STR 25 + 2Ï¿½. DAMAGE MEASURES 1.10Ï¿½ L X 0.007Ï¿½ W X 0.006Ï¿½ D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01639 REV IR DATED 5/24/2021.

Part: SKIN — DENTED (FS 640) · airframe 37,073 hrs · 35,778 cycles

AFT FUSELAGE SKIN DENT FS 640.00 - 2Ï¿½ LH STR 26 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENT AT AFT FUSELAGE FS640.00 - 2Ï¿½ LH STR 26 +2Ï¿½.DAMAGE MEASURES 0.550Ï¿½L X 0.500Ï¿½W X 0.008Ï¿½D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01636 REV A DATED 5/22/2021.

Part: SKIN — DENTED (FS 640) · airframe 37,073 hrs · 35,778 cycles

AFT FUSELAGE SKIN DENT FS 640.00 - 1Ï¿½ LH STR 26 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED SKIN DENT AT AFT FUSELAGE FS640.00 - 1Ï¿½ LH STR 26 +2Ï¿½. DAMAGE MEASURES 1.200Ï¿½L X 0.600Ï¿½W X 0.023Ï¿½D. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01636 REV A DATED 5/22/2021.

Part: SKIN — DENTED (BS 682 S24R) · airframe 37,073 hrs · 35,778 cycles

AFT FUSELAGE SKIN DENT FS682.0 + 9Ï¿½ RIGHT HAND STRINGER 24 + 2Ï¿½. ***AIRCRAFT REMOVED FROM SERVICE*** HAND FORMED DENT AT FS682.0 + 9Ï¿½ RIGHT HAND STRINGER 24 + 2Ï¿½, DIMENSION0.700Ï¿½L X 0.500Ï¿½W X 0.050Ï¿½W. DENT FOUND TO BE OUT OF LIMITS REF CRJ200 SRM 53-00-31. HFEC PERFORMED WITH NO INDICATIONS. RESTORED SURFACE FINISH. ALL WORK PERFORMED AND WITHIN LIMITS IAW ASAP EA # AWAC-CRJ253-1635 REV IR DATED 5/21/2021.

Part: BULKHEAD — CRACKED (FS 621) · airframe 37,073 hrs · 35,778 cycles

CRACK INDICATIONS (7 TOTAL) AT FS621.00 AFT PRESSURE WEB. CRACKS AT THE FOLLOWING LOCATIONS, WL 128.5 - 131.2, LBL 18.0, CRACK LENGTH 2.7"L, WL 113.5 - 114.2, LBL 9.50, CRACK LENGTH 0.7"L, 109.5 - 112.0, BL 0.0, CRACK LENGTH 2.5"L, WL 110.5 - 111.2, RBL 9.50, CRACK LENGTH 0.7"L, WL 128.5 - 129.0, RBL 18.0, CRACK LENGTH 0.5"L, WL 110.5 - 111.8, RBL 18.0, CRACK LENGTH 1.3"L, WL 109.5 - 110.0, RBL 27.5, CRACK LENGTH 0.5"L. ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED FS621.00 AFT PRESSURE WEB, PERFORMED HFEC WITH NO INDICATIONS, RESTORED PROTECTIVE FINISHES. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-53-61-1240 REV D, DATED 2016-10-31 AND REO 601R-53-61-7648 REV INITIAL ISSUE DATES 2021-06-03.

Part: RVDT — FAILED (NLG STEERING) · airframe 36,362 hrs · 35,019 cycles

RECIEVED A STEERING INOPERATIVE CAUTION MESSAGE AFTER RETRACTING GEAR, COMPLIED WITH QRH, MESSAGE REMAINED, RETURNED TO DEPARTURE, LANDED NORMAL USING DIFFERENTIAL BREAKING. NO HYD SYST 3 MESSAGE, NO OTHER EICAS MESSAGES, NO STEERING ON TAXI AFTER LANDING. AIRCRAFT REMOVED FROM SERVICE, TROUBLESHOT AND FOUND THE LT RVDT HARD FAILURE. R & R THE LT STEERING RVDT IAW AMM 32-51. OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 35,102 hrs · 33,832 cycles

NOSE GEAR WOULD NOT RETRACT AFTER T/O. EICASE SHOWED NOSE GEAR DOWN AND NOSE GEAR OPEN INDICATIONS. RAN QRH. SELECTED GEAR DOWN. GEAR EXTENDED AND NORMAL LANDING.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,453 hrs · 33,242 cycles

FOUND INDICATION AT FS 409.00+128 OTBD RBL 18 POST AFT FLANGE RADIUS APPROX .250" LONG FSH FAILS NDT.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 34,453 hrs · 33,242 cycles

AC GROUND POWER RECEPTACLE STRUCTURE CRACKED @ MOUNT FASTENERS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 34,453 hrs · 33,242 cycles

INDICATION NOTED AT FS621 REAR PRESSURE BULKHEAD FWD FACE AT BL0.00, WL 131 APROX 7.5" LONG AND 53% FULL SCREEN HEIGHT FAILING NDT.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,453 hrs · 33,242 cycles

RT WALL SEAT TRACK IS CORRODED AT FS 409+128.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,453 hrs · 33,242 cycles

RT F.S.484 CLIP IS CRACKED AT RBL27.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,453 hrs · 33,242 cycles

RT WALL SEAT TRACK IS CORRODED AT F.S.513.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,453 hrs · 33,242 cycles

RT WALL SEAT TRACK IS CORRODED AT F.S.513.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 34,453 hrs · 33,242 cycles

INTERCOSTAL CORRODED BETWEEN F.S.349.00 AND F.S.364.00, STRG 26L AND 27.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,453 hrs · 33,242 cycles

LT SIDEWALL SEAT TRACK IS CORRODED AT FS 529.00.

Part: VANE — CHAFED (TE FLAP) · airframe 34,453 hrs · 33,242 cycles

LT WING OUTBOARD FLAP FIXED VANE IS CHAFED AT W.S.274.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,453 hrs · 33,242 cycles

LT WALL SEAT TRACK IS CORRODED AT VF.S.409+128.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,453 hrs · 33,242 cycles

FOUND INDICATIONS AT FS 409+128 B.L.0.00 LT AND RT POSTS AFT FLANGE RADIUS APPROX. .500" LONG 100% FSH BOTH FAIL NDT.

Part: POST — CRACKED (FUSELAGE) · airframe 34,453 hrs · 33,242 cycles

FOUND INDICATIONS AT FS409+128 BL 0 LT AND RT POSTS AFT FLANGE RADIUS APPROX. .500" LONG 100% FSH BOTH FAILS NDT.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 32,812 hrs · 31,665 cycles

DURING TAKEOFF, THE FLAPS FAILED AT 3 DEGREES WHEN SELECTING FLAPS FROM 0 TO 8. RAN QRH, RETURNED TO DEPARTURE, EMERGENCY WAS DECLARED. AFTER LANDING FLAPS SYSTEM WAS SUCCESSFULLY RESET IAW 98-018G.

Part: STIFFENER — CRACKED (BS 340) · airframe 32,615 hrs · 31,462 cycles

PAX DOOR MOTOR FOUND CRACKED IN THE LOWER VERTICAL STIFFENER. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-42-06, AND 51-42-13.

Part: PIN — PULLED (EMERGENCY LIGHTS) · airframe 32,332 hrs · 31,172 cycles

4182 EMERGENCY PATH LIGHTING FROM ROW 5 TO 8 INOP. FOUND PIN PULLED OUT OF ENVIRONMENTAL SPLICE AT ROW 7. R&R'D PIN IAW ESPM 20-17, FUNCTION CHECK GOOD.

Part: LIGHT — INOPERATIVE (ROW 5) · airframe 32,168 hrs · 30,994 cycles

4231 EMERGENCY LIGHTS ROW 5 INOP ON FLOOR. PLACARDED & PLACED ON MEL. REMOVED & REPLACED EMERGENCY LIGHT STRIP ROW 5 IAW 33-51 & AWAC SUPP 16-371A. OPS CHECK GOOD.

Part: FRAME — CORRODED (BS 409) · corrosion level 2 · airframe 31,470 hrs · 30,320 cycles

FRAME BS 409+16 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGERS 26R AND 26L

Part: FRAME — CORRODED (BS 349) · corrosion level 2 · airframe 31,470 hrs · 30,320 cycles

FRAME BS 349 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGER 26L AND 26R.

Part: FITTING — CORRODED (BS 618) · corrosion level 2 · airframe 31,470 hrs · 30,320 cycles

LBL 27 AFT FITTING IS CORRODED AT OTBD NUTPLATE LOCATION AT BS 618.

Part: FRAME — CRACKED (BS 333) · airframe 31,470 hrs · 30,320 cycles

FRAME BS 333 CRACKED AT STRINGER 2L.

Part: STRINGER — CRACKED (BS 379) · airframe 31,470 hrs · 30,320 cycles

STRINGER 3L CRACKED AT BS 379.

Part: BRACKET — CRACKED (BS 621) · airframe 31,470 hrs · 30,320 cycles

RIGHT INTERCOSTAL BRACKET CRACKED ON THE AFT REAR PRESSURE BULKHEAD AT BS 621. REPLACED INTERCOSTAL IAW SRM 51-41-21.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 31,470 hrs · 30,320 cycles

FLIGHT DECK FLOORBEAM CRACKED ON THE FWD SIDE OF BS 280, RBL9. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-06, AND 51-42-21.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 31,470 hrs · 30,320 cycles

PAX DOOR EDGE MEMBER HAS A CRACK ON FWD END. REPAIRED IAW REO 601R-52-11-279, REV NC.

Part: RETAINER — CRACKED (PANEL SEAL) · airframe 31,470 hrs · 30,320 cycles

SEAL RETAINER CRACKED ON PANEL 422BT. REPAIRED THE SEAL RETAINER IAW SUP 16-363.

Part: ENGINE — POWER LOSS (RIGHT) · airframe 31,344 hrs · 30,210 cycles

AT 31,000 FEET LOST 5% N1 ON RIGHT ENGINE WITH SLIGHT YAW. LASTED 2-3 SECONDS, THEN CONDITION CORRECTED ITSELF WITH NO INPUT FROM THE CREW. N1 WAS SET TO 85 % AT TIME OF ROLLBACK, AND SPEED SWITCHES WERE SELECTED ON. NO ABNORMAL CAUTIONS OR MESSAGES PRESENT DURING ROLLBACK. THE REST OF THE FLIGHT WAS UN-EVENTFUL, DECLARED EMERGENCY. DID NOT NOTICE FLUXUATION IN ANY OTHER SETTINGS OR PERAMETERS. DURING POWER ASSURANCE RUN AND ACCELERATION, DECELERATION CHECK NOTED AND AUDIBLE HISSING OR BLOWOFF NOISE FROM RIGHT ENGINE.

Part: FLAP SYSTEM — MALFUNCTIONED (WING) · airframe 30,428 hrs · 29,363 cycles

FLAPS FAIL DURING CLIMB OUT, AT FLT LEVEL 230, 280 KNOTS FLAPS AT 0 WITH NO MOVEMENT OR SELECTION TO FLAPS. COMPLIED WITH QRH, MESSAGE PERSISTED. DIVERTED AND DECLARED EMERGENCY. RESET FLAPS IAW FIM 27-50-00 AND SET FLAPS AT 20 DEGREES.

Part: FLAP — MALFUNCTIONED (WING) · airframe 30,424 hrs · 29,358 cycles

FLAP FAIL CAUTION MESSAGE DURING CRUISE CLIMB, FLAPS AT ZERO DEGREES, PERFORMED FLAP RESET PROCEDURE IAW SUPP 98-18G, BOX 12, FLAPS RESET. NOTED BY MAINTENANCE.

Part: UNKNOWN — SMOKE (CARGO BAY) · airframe 29,862 hrs · 28,849 cycles

CARGO SMOKE WARNING OCCURRED AT GATE. RAMP VERIFIED SMOKE PRESENT IN CARGO BAY WHEN OPENING DOOR.

Part: THRUST REVERSER — LACK OF LUBE (RT ENGINE) · airframe 29,274 hrs · 28,299 cycles

IN FLIGHT RECEIVED RT REV UNLOCK MSG. COMPLIED WITH QRH. DIVERTED & LANDED BELOW 47000 LBS & MAX BTMS WAS 4454. DEACTIVATED RT TR IAW SUP 15-046, M ACTION COMPLIED WITH. PERFORMED TR LUBE IAW SUPP 14-118A. OPERATIONS CHECKED GOOD AT THIS TIME. REMOVED PLACARD & FROM MEL.

Part: ADG — DEPLOYED · airframe 29,145 hrs · 28,175 cycles

FLIGHT NR 4026, IMMEDIATELY AT TAKEOFF, LOUD NOISE FROM FRONT OF ACFT, NO CAUTIONS, OR WARNINGS. ELEC SYNOPTIC SHOWED ADG DEPLOYED. ADG DEPLOYED AT APPROX 145 KNOTS, MAX OF 200 KNOTS ON RETURN. ADG DEPLOYED APPROX 14 MINUTES. PERFORMED VISUAL INSPECTION OF ADG STRUT & GEN HOUSING IAW SUPP 10-066. NO DEFECTS NOTED AT THIS TIME STOWED ADG IAW SUPP 16-015, IAW 253890 2 FOR ADG AUTO DEPLOY MEL & 253890 3 FOR NDT MEL.

Part: COMPUTER — FAILED (COCKPIT) · airframe 28,057 hrs · 27,120 cycles

FLIGHT 9365, 3848CXL 3951 CBP1 N5 & CBP2 H14 POPPED. ELEC BURNING SMELL IN COCKPIT & GALLEY. AHRS WAS INTERMITTENT THEN HARD FAIL. R & R AHRS COMPUTER. OPERATIONS CHECKED GOOD IAW AMM 34-21-01. CB DID NOT POP OR ELEC ODOR NOTED AT THIS TIME. SN OFF 3393 & SN ON 3253.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,418 hrs · 26,477 cycles

FLIGHT NR 3849, EMER FLOOR LIGHT STRIP INOPERATIVE AFT OF ROW 8.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 27,405 hrs · 26,467 cycles

FS 280 STRINGER 3L CLIPS ARE CRACKED.

Part: STIFFENER — CRACKED (RT WING) · airframe 27,405 hrs · 26,467 cycles

WING STIFFENER IN RT WW AT WS 48 IS CRACKED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 27,405 hrs · 26,467 cycles

UPPER CAP ON FS 280 FLOORBEAM IS CRACKED AT RBL 9 & 12.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,405 hrs · 26,467 cycles

LEFT AFT FUSELAGE SKIN HAS PROTRUDING DENT AT FS 712.00.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,405 hrs · 26,467 cycles

LT UPPER OBLIQUE ANGLE ON SF621 BULKHEAD CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,405 hrs · 26,467 cycles

OUTER CLIP CRACKED AT FS 280 LBL 9, BOTH CLIPS CRACKED AT LBL 9.

Part: FITTING — CHAFED (HORIZ STAB) · airframe 27,405 hrs · 26,467 cycles

HORIZONTAL STAB LT & RT OTBD PIVOT FITTING ON STAB IS GOUGED & SCORED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 27,405 hrs · 26,467 cycles

55378-8000-0016 PAX DOOR AFT DRAG ANGLE IS CRACKED.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 27,405 hrs · 26,467 cycles

BRACK TRANSDUCER BRACKET IN LT WW IS CRACKED.

Part: STRUCTURE — CRACKED (NLG WW) · airframe 27,405 hrs · 26,467 cycles

NOSE WW CUT OUT AFT RT CORNER IS CRACKED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,405 hrs · 26,467 cycles

FS 202 BULKHEAD CRACKED APPROX 3" LONG AT CUT OUT FOR PARKING BRAKE CABLE.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 27,405 hrs · 26,467 cycles

PAX DOOR INNER HANDLE CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,405 hrs · 26,467 cycles

LEFT WINDSHIELD POST LOWER FITTING IS CRACKED.

Part: SEAL DEPRESSOR — GOUGED (FUSELAGE) · airframe 27,405 hrs · 26,467 cycles

SERVICE DOOR SEAL STRIKER GOUGED.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 27,405 hrs · 26,467 cycles

LOWER SUPPORT ANGLE FOR CARGO COMPARTMENT CURTAIN HANGAR SUPPORT ON AFT END HAS A CRACK ON OTBD END.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,405 hrs · 26,467 cycles

RIGHT FS 484.00 CLIPS ARE CRACKED AT BL 27.00.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,405 hrs · 26,467 cycles

FLIGHT COMPARTMENT RT SIDE WINDOW POST LOWER FITTING IS CRACKED.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 26,908 hrs · 25,992 cycles

EMERGENCY LIGHT FLOOR TRACK COVER AT ROW 1C - D COMING OFF.

Part: ENGINE — FAILED (APU) · airframe 25,641 hrs · 24,768 cycles

APU AUTOSHUTDOWN FLAME OUT. FIRST OFFICER FOUND METAL DEBRIS NEAR APU EXHAUST. INSPECTED & FOUND INTERNAL APU FAILURE, CLEANED & SECURED AREA. APU IS CONSIDERED INOPERABLE.

Part: SKIN — DAMAGED (BS 227) · airframe 23,043 hrs · 22,267 cycles

SKIN HAS ONE SCREW HOLE THAT ELONGATED AT THE 12:00 POSITION. REPAIRED RT FUSELAGE SKIN IAW REO 601R-53-11-2529, REV B.

Part: SKIN — DAMAGED (BS 227) · airframe 23,043 hrs · 22,267 cycles

SKIN SURROUNDING PANEL 132AL HAS TWO PLACES THAT HAS SCREW BITE MARKS. BLENDED OUT DAMAGE ON RT FUSELAGE SKIN IAW REO 601R-53-11-2529, REV B.

Part: MOUNT — CRACKED (FUSELAGE) · airframe 23,043 hrs · 22,267 cycles

SERVICE DOOR SWITCH MOUNT IS CRACKED. R & R MOUNT ON SERVICE DOOR IAW SRM 51-41-02 AND 51-42-21.

Part: SKIN — CRACKED (RUDDER) · airframe 23,043 hrs · 22,267 cycles

RUDDER RT LOWER FWD SKIN IS CRACKED AND DENTED. R & R SKIN.

Part: TIE DOWN — CORRODED (BULKHEAD) · corrosion level 2 · airframe 23,043 hrs · 22,267 cycles

BULKHEAD TIE DOWNS AT 559+80 LBL 9 AND 27 AND RBL 9 AND 27 HAVE CORROSION. BLENDED OUT OF LIMITS, R & R.

Part: HEAT SHIELD — DAMAGED (BS 683-735) · airframe 23,043 hrs · 22,267 cycles

APU AFT HEAT SHIELD HAS SIX SCREWS PULLED THRU. FABRICATE AND INSTALLED HEAT SHIELD IAW SRM 51-24-16, SRM 51-21-11,SRM 51-25-06 AND SRM 51-40-11.

Part: BULKHEAD — CHAFED (BS 280) · airframe 23,043 hrs · 22,267 cycles

RT AFT FS 280 BULKHEAD CHAFED. REPAIRED IAW REO 601R-53-11-1727. REV E.

Part: TRUNNION — DAMAGED (MLG) · airframe 23,043 hrs · 22,267 cycles

DURING COLD WORKING OF MLG FOUND TWO OVERSIZED HOLES 1 ON LT & 1 ON RT LOWER MLG TRUNNION FLANGE. REPAIRED DISCREPANT HOLES ON LT & RT MLG TRUNNION FLANGE. IAW REO 601R-57-21-1963.

Part: SILL — CORRODED (BS 319-349) · corrosion level 2 · airframe 23,043 hrs · 22,267 cycles

PAX DOOR LOWER SILL HAS MULTIPLE AREAS OF CORROSION FOUND TO BE OUT OF ALLOWABLE LIMITS. R & R PAX DOOR LOWER SILL IAW SRM.

Part: BRACKET — GOUGED (RT NACELLE) · airframe 23,043 hrs · 22,267 cycles

GOUGE ON UPPER T/E BRACKET ON RT PYLON L/E PANEL 421 AL IS OUT OF LIMITS DUE TO PROXIMITY TO FASTENER HOLE. R & R.

Part: PANEL — CHAFED (FUSELAGEWING) · airframe 23,043 hrs · 22,267 cycles

VISOR PANEL NR 326 BL DISTORTED (BENT) CHAFED BEYOND LIMITS. REPLACED WITH SERVICEABLE VISOR PANEL.

Part: SEAL — CRACKED (SPOILER) · airframe 23,043 hrs · 22,267 cycles

LT FLIGHT SPOILER WING T/E SEAL IS CRACKED. R & R.

Part: VANE — CRACKED (RT WING TE FLAP) · airframe 23,043 hrs · 22,267 cycles

RT FLAP VANE L/E CRACKED. BLENDED 2 AREAS WITHIN LIMITS BLENDED INBD L/E OUT OF LIMITS CHANGED INBD L/E SKIN.

Part: SKIN — CHAFED (FUSELAGE) · airframe 23,043 hrs · 22,267 cycles

INNER SKIN CHAFED OUT OF LIMITS. REPLACED INNER SKIN.

Part: SUPPORT BRACKET — CRACKED (BS 589) · airframe 23,043 hrs · 22,267 cycles

FWD LOWER SUPPORT BRACKET FOR CARGO BAY DOOR WAS CRACKED. R & R IAW SRM 51-42-06 & 51-41-02.

Part: SKIN — CHAFED (WING) · airframe 23,043 hrs · 22,267 cycles

CHAFED L/E SKIN AT FLA STA 60.005 FOUND TO BE OUT OF LIMITS 040 MATERIAL LOSS ORIG THICK 050" REM MATERIAL 010" MAX ALLOWED 025" IAW REO 601R-57-52-004, REV C. R & R L/E SKIN IAW SRM 51-40-11 & SRM 51-42-13.

Part: STRUCTURE — CORRODED (BS 574) · corrosion level 2 · airframe 23,043 hrs · 22,267 cycles

CORROSION FOUND OUT OF LIMITS AT FS 574+10 LBL 9. R & R IAW SRM 53-61-49.

Part: ANGLE — CRACKED (BS 484) · airframe 23,043 hrs · 22,267 cycles

ANGLE IS CRACKED. REMOVE UNSERVICEABLE ANGLES REPLACED WITH NEW IAW REO 601R-53-41-059, REV B.

Part: BRACKET — CRACKED (MLG) · airframe 23,043 hrs · 22,267 cycles

BRAKE PRESSURE TRANSDUCER BRACKET IN RT WHEEL WELL IS CRACKED. R & R RT BRAKE PRESSURE TRANSDUCER BRACKET, PN 601R75262-157 IAW SRM 51-42-06.

Part: WIRE HARNESS — DEFECTIVE (NLG) · airframe 21,393 hrs · 20,684 cycles

WHEN GEAR SELECTED TO DOWN NLG DOORS WERE OPENING AND CLOSING RAPIDLY LONGER THAN NORMAL TIME FOR GEAR TO INDICATE DOWN AND LOCKED. INTEROGATED PSEU, FOUND SENSOR S35 FAULT-NGD LK2 REF 237682/2 FOR MEL. REPLACED NLG DOWNLOCK TO PROX SENSOR HARNESS ASSY PER AMM 32-61-05. GEAR INDICATION SATISFACTORY AND OPS CHECK GOOD. REMOVED MEL REMOVAL PLACARD. RII I-165

Part: WIRE HARNESS — FAULTY (ANTI-SKID SYS) · airframe 21,217 hrs · 20,515 cycles

ANTISKID OUTBOARD CAUTION MESSAGE AT 30KTS. ABORTED TAKEOFF. BTMS MAX READING 3, 3, 3, 3. REMOVED AND REPLACED LEFT OUTBAORD ANTISKID HARNESS.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 21,217 hrs · 20,515 cycles

ANTISKID CAUTION AT 75KTS, ABORTED TAKEOFF. BTMS MAX READINGS 2, 5, 5,7. HIGH ENERGY STOP INSPECTION NOT REQUIRED PER MXC. WHEN THROTTLES AT IDLE MESSAGE CLEARED AND RECEIVED MOMENTARY CONFIG SPOILERS WARNING. NO WARNING PRESENT NOW.

Part: UNKNOWN — ODOR (CABIN) · airframe 18,383 hrs · 17,640 cycles

BURING ODOR NOTED AROUND ROWS 6-7. ALL OVERHEAD LIGHT ARE OFF. NO BURNING ODOR NOTED AROUND ROW 6-7. ACFT OK FOR SERVICE IAW AMM 25-20.

Part: SILL — CORRODED (BS 574-621) · corrosion level 2 · airframe 18,377 hrs · 17,635 cycles

CORROSION ON LT CARGO FLOOR SILL BY CARGO DOOR. REMOVED, FABRICATED, AND INSTALLED NEW LT CARGO FLOOR SILL.

Part: RISER — CRACKED (PAX DOOR) · airframe 18,377 hrs · 17,635 cycles

PAX DOOR FWD STEP RISER CRACKED. REPAIRED PAX DOOR, FWD STEP RISER AT 2ND STEP IAW REO 601R-52-11-702, REV E ZONE 2.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 18,377 hrs · 17,635 cycles

SEAT TRACKS AT LBL 9 & RBL 9 AT FS 539+112 IN CARGO BAY ARE CORRODED TABLE R & R SEAT TRACKS.

Part: BRACKET — CRACKED (BS 409) · airframe 18,377 hrs · 17,635 cycles

HYD LINE BRACKET IN RT WHEEL WELL CRACKED. R & R HYD LINE BRACKET ON RT WHEEL WELL IAW SRM 51-42-06.

Part: FITTING — CHAFED (LT AILERON) · airframe 18,377 hrs · 17,635 cycles

LT AIRLERON FLUTTER DAMPER SHEAR LINK ATTACH POINT ON AILERON IS CHAFED ON OTBD SIDE. REPAIRED DAMAGE IAW REO 601R-57-61-367 DAMAGE DEPTH .060.

Part: HEAT SHIELD — LOOSE (BS 682) · airframe 18,377 hrs · 17,635 cycles

APU EXHAUST AFT HEAT SHIELD HAS LOOSE FASTENERS AND 2 EA PULLED THRU FASTENERS. REPAIRED APU AFT EXHAUST HEAT SHIELD IAW REO 601R-49-81-051.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 18,377 hrs · 17,635 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED CRACKED AFT DRAG ANGLE SECTION THEN INSTALLED NEW SERVICEABLE SECTION IAW REO 601R-52-11-513, REV A.

Part: FITTING — CRACKED (BS 460) · airframe 18,377 hrs · 17,635 cycles

BOTH TUB FITTING CRACKED AT 460 AND RBL9. REMOVED UNSERVICEABLE FITTING AND INSTALLED SERVICEABLE FITTING IAW SRM 51-42-21.

Part: FITTING — CRACKED (BS 484) · airframe 18,377 hrs · 17,635 cycles

FS 484, LBL 9 HAS A CRACKED BAT TUB FITTING IN AFT RADIUS. REMOVED UNSERVICEABLE FITTING AND INSTALLED SERVICEABLE FITTING IAW SRM 51-42-21.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 18,377 hrs · 17,635 cycles

RT MLG DOOR CHAFED 2EA PLACES. REPAIRED IAW REO`S 601R-52-82-102 & 601R-52-82-034.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 18,377 hrs · 17,635 cycles

FS 484, CLIP CRACKED AT RBL 36. REMOVED UNSERVICEABLE CLIP AND REPLACED WITH SERVICEABLE CLIP IAW REO 601R-53-41-059, REV B.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 18,377 hrs · 17,635 cycles

PAX DOOR ASSIST MOTOR MOUNTING BRACKET CRACKED. REMOVED CRACKED POWER ASSIST MOTOR SUPPORT ANGLE, THEN INSTALLED NEW SERVICEABLE SUPPORT ANGLE, IAW SRM 51-40-11, 51-42-06.

Part: SKIN — CHAFED (LT AILERON) · airframe 18,377 hrs · 17,635 cycles

LT AILERON UPPER L/E SKIN CHAFED. REPAIR CHAFED AREA IAW REO 601R-57-60-013.

Part: SKIN — CHAFED (RT AILERON) · airframe 18,377 hrs · 17,635 cycles

RT AILERON UPPER L/E SKIN CHAFED. REPAIR CHAFED AREA IAW REO 601R-57-60-013.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 18,377 hrs · 17,635 cycles

PAX DOOR OUTER HANDLE CRACKED. REMOVED CRACKED OUTER HANDLE AND INSTALLED NEW SERVICEABLE OUTER HANDLE IAW EO E08/007/452, REV A.

Part: INTERCOSTAL — CRACKED (BS 621) · airframe 18,377 hrs · 17,635 cycles

CRACKED INTERCOSTAL ADJACENT TO STRINGER 14 . REMOVED AND REPLACED IAW REO 601R-53-61-100.

Part: PANEL — CRACKED (LT NACELLE) · airframe 18,377 hrs · 17,635 cycles

LT ENGINE LOWER NOSE COWL THRUST REVERSER PDU ACCESS DOOR VENT LOUVER CRACKED. R & R VENT IAW SRM 51-42-13.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 18,377 hrs · 17,635 cycles

PITTING CORROSION ON NR 2 RT SIDE SEAT TRACK. R & R RT NR 2 SIDE SEAT TRACK.

Part: CONTROL LEVER — FAILED (TE FLAPS) · airframe 15,414 hrs · 14,479 cycles

AFTER T/O, FLAPS FAILED AT 20 DEGREES. COMPLIED WITH QRH. PERFORMED FLAP RESET PROCEDURE IAW SUPP 98-18D, BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. PERFORMED OPS TEST OF FLAPS SYS IAW AMM 27-51-05. ALL CHECKS GOOD, REMOVED FROM MEL. M/C REF 201889/1 FOR R & R OF FLAP CONTROL LEVER IAW AMM 27-51-01 ALL CHECKS GOOD. REF 201889/1 - R & R FLAP CONTROL LEVER OPS CK IAW 27-51-01. ALL CKS GOOD.

Part: BRACKET — CRACKED (BS 280) · airframe 13,571 hrs · 12,611 cycles

CRACKS FOUND ON BRACKETS AT FS 280.00, LBL 9 INBD AND OTBD. BRACKET AT FS 280.00, LBL9 REPLACED IAW SRM 51-42-06 AND 51-42-20. (K)

Part: ATTACH FITTING — CRACKED (BS 280) · airframe 13,571 hrs · 12,611 cycles

CRACK FOUND ON FS 280 RBL 9 INBD AND OTBD CLIP. 2 CLIP REPLACED IAW SRM 51-42-20 AND 51-42-06. (K)

Part: BULKHEAD — CRACKED (BS 280) · airframe 13,571 hrs · 12,611 cycles

CRACK FOUND ON PILOT BULKHEAD FS 280, RBL 9, LWR FLANGE. PILOT BULKHEAD REPAIR IAW REO 601R-53-11-171, REV D. (K)

Part: ANGLE — CRACKED (BS 280) · airframe 13,571 hrs · 12,611 cycles

CRACK ON PILOT BULKHEAD AFT ANGLE FS 280 LBL 9. REPAIRED IAW REO 601R-53-11-138. (K)

Part: BULKHEAD — DAMAGED (BS 280) · airframe 13,571 hrs · 12,611 cycles

SCRATCH REPAIR ON FS 280 PILOT BULKHEAD RBL 9, WL 94.50 IAW REO 601R53-11-1706. (K)

Part: ANGLE — DAMAGED (BS 280) · airframe 13,571 hrs · 12,611 cycles

CRACK FOUND ON PILOT BULKHEAD FS 280, LBL 9 LWR FLANGE (CRACK LENGTH .750). REPAIR ON PILOT BULKHEAD AT FS 280, LBL 9 LWR FLANGE CARRIED OUT IAW REO 601R-53-11-171. (K)

Part: THRESHOLD — CORRODED (BS 319-349) · airframe 13,571 hrs · 12,611 cycles

SERVICE DOOR THRESHOLD PLATE FOUND CORRODED OUT OF LIMIT. SERVICE DOOR THRESHOLD PLATE REPLACED IAW SRM 51-41-02. (K)

Part: PRESSURE BLKHD — CRACKED (BS 621) · airframe 13,571 hrs · 12,611 cycles

AFT PRESSURE BULKHEAD CRACKED AT LINTEL FITTING LOCATION. REPAIRED IAW REO 601R-53-61-1230. (K)

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 13,571 hrs · 12,611 cycles

RT HYD MANIFOLD SUPPORT BRACKET IN AFT EQUIPMENT COMPT CRACKED (AFT LWR AREA) .20 INCH LONG RT HYD MANIFOLD SUPPORT BRACKET REPLACED IAW REO 601R-53-62-031, REV A. (K)

Part: ACM — SEIZED (LEFT) · airframe 12,696 hrs · 11,745 cycles

REPORTS NR 1 PACK SMELLS HOT IN AUTO AND MANUAL IN FLIGHT AND ON THE GROUND AND DUCT TEMP UNCONTROLLABLE. FOUND CONNECTOR PLUGS S3HG AND P9HG BROKEN, PLACED NR 1 PACK ON MEL AND PLACARDED. FOUND ACM SEIZED REMOVED AND REPLACED ACM IAW AMM 21-00. OPS CHECK GOOD. REMOVED PLACARD MEL. (K)

Part: HANDLE — MALFUNCTIONED (MLG) · airframe 12,495 hrs · 11,549 cycles

AFTER GEAR RETRACTION, GEAR STAYED IN DOWN POSITION, ASSOCIATED MESSAGES WERE INBD ANTISKID INOP AND PARK BRAKE SOV CAUTION MESSAGES. AFTER CYCLING GEAR, GEAR RETRACTED AND CYCLED NORMALLY. REMOVED AND REPLACED LANDING GEAR HANDLE IAW AMM 32-31-01. OPS CHECK GOOD. (K)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 11,408 hrs · 10,523 cycles

FLAPS FAILED AT 20 DEGREES WITH FLAPS FAIL CAUTION AFTER TAKEOFF. LANDED AT FLAPS 20 AFTER COMPLYING WITH QRH. COMPLIED WITH AWAC SUPP 98-018B RESET, FLAPS RESET OK. RESET.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 10,925 hrs · 10,080 cycles

FLAPS FAILED AT 30 DEGREES ON APPROACH, COMPLIED WITH QRH LANDED IN BUF. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4 FLAPS SYSTEMS RESET OK. (A)

Part: TARGET — LOOSE (LT MLG) · airframe 10,452 hrs · 9,634 cycles

LT MLG DID NOT RETREAT AFTER TAKEOFF GEAR DISAGREE MSG C/W QRH RETURN TO LGA AT WS 39800 LBS. FOUND LT UPLOCK TARGET LOOSE AND OUT OF ADJUSTMENT. ADJUSTED TARGET FOR LT MLG UPLOCK. REF AMM 32-32-05. OPS TEST OF LANDING GEAR EXTENTION AND RETRACTION SYSTEM NORMAL. REMOVED FROM MEL.

Part: CONTROL UNIT — FAULTED (SPOILER) · airframe 9,060 hrs · 8,341 cycles

INFLIGHT RECEIVED SPOILERON FAULT YELLOW CAUTION MESSAGE AND IB AND OB GROUND SPOILER FAULT STATUS MESSAGES. COMPLIED WITH QRH (FERRY TO PHL). INTERROGATED SECU NR 1 AND SECU NR 2 FAULT LOG FOUND CODE 13 (SECU 1 MODULE A) REMOVED AND REPLACED SECU NR 1 IAW 27-61-05. OPS CHECK GOOD IAW 27-61-00. (K)

Part: YOKE — LOOSE (COCKPIT)

UNUSUAL NOISE HEARD WHEN FIRST OFFICER YOKE TURNED. MORE NOTICEABLE WHEN TURNED RIGHT. ALSO NOTED THROUGH FLOOR ON CAPTAINS SIDE. RETORQUED FIRST OFFICERS YOKE REF SB CRJ-SL-27-045 REV A AND M 27-11-01. OPERATIONAL CHECK GOOD. (M)

Part: FLOORBEAM — CRACKED (BS 621)

FOUND RIGHT FS 621 FLOOR SUPPORT ANGLE CRACKED. (M) MAINTENANCE REPAIRED IAW REO 601R-53-61-117. (M)

Part: FLOORBEAM — CRACKED (BS 621)

FOUND LEFT FS 621 FLOOR SUPPORT ANGLE CRACKED. (M) MAINTENANCE REPAIRED IAW REO 601R-53-61-117. (M)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 8,615 hrs · 7,906 cycles

LT WING LOWER PLANK ACCESS HOLE NR 1 540BB HAS MINOR CORROSION IN NON-CRITICAL AREAS APPROX .003 INCH DEEP AND 5 INCH LONG IN (2) PLACES. (K) MAINTENANCE REPAIRED IAW REO 601R-57-21-030. (M)

Part: SKIN — CORRODED (RT WING) · corrosion level 1 · airframe 8,615 hrs · 7,906 cycles

RT WING LOWER PLANK ACCESS HOLE NR 1 640BB HAS MINO CORROSION IN NON-CRITICAL AREAS APPPROX .003 DEEP AND 2.5 INCH LONG IN (2) PLACES. (K) MAINTENANCE REPAIRED IAW BSC REO 601R-57-21-030 REV F. (M)

Part: SKIN — GOUGED (TE FLAP) · airframe 8,615 hrs · 7,906 cycles

RT WING IB FLAP LOWER SKIN GOUGED/DENTED APPROX 3 INCHES LONG X 3 INCHES WIDE X .205 INCH DEEP, ADJACENT TO RIB AT WS 74.8, APPROX 8 INCHES AFT OF LEADING EDGE OF FLAP. (K) MAINTENANCE REPAIRED FLAP LOWER SKIN IAW BSC EO 601R-57-12572. (M)

Part: SKIN — CORRODED (LT WING) · corrosion level 1 · airframe 8,615 hrs · 7,906 cycles

LT WING PLANK LOWER ACCESS HOLE NR 2 510AB HAS MINOR CORROSION IN NON-CRITICAL AREAS APPROX .005 DEEP AND 5 INCHES LONG. (K) MAINTENANCE REPAIRED IAW REO 601R-57-21-030. (M)

Part: ANGLE — CRACKED (BS 484) · airframe 8,615 hrs · 7,906 cycles

LT 484 ANGLE IS CRACKED AT LBL 36 APPROX .5 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0030A. (M)

Part: ANGLE — CRACKED (BS 484) · airframe 8,615 hrs · 7,906 cycles

LT 484 ANGLE IS CRACKED AT LBL 27 APPROX .5 INCHES LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0029B. (M)

Part: ANGLE — CRACKED (BS 484) · airframe 8,615 hrs · 7,906 cycles

RT 484 ANGLE IS CRACKED AT RBL 27 APPROX 1 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0029B. (M)

Part: ANGLE — CRACKED (BS 484) · airframe 8,615 hrs · 7,906 cycles

RT 484 ANGLE IS CRACKED AT RBL 36 APPROX .25 INCH LONG. (K) MAINTENANCE REPAIRED ANGLE IAW BOMBARDIER REO 601R-53-41-059 REV A AND BOMBARDIER STANDARD REPAIR 601R-53-0030A. (M)

Part: BRACKET — CRACKED (RT MLG WW) · airframe 8,615 hrs · 7,906 cycles

HYDRAULIC PRESSURE BRACKET IS CRACKED APPROX .1 INCH LONG IN RT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED AND REPLACED HAT CHANNEL P/N 601R75262-157 IAW CRJ 200 SRM 51-42-06. (M)

Part: CHANNEL — CRACKED (LT MLG WW) · airframe 8,615 hrs · 7,906 cycles

HYDRAULIC PRESSURE TRANSDUCER HAT CHANNEL CRACKED APPROX .1 LONG IN LT MLG WHEEL WELL CEILING. (K) MAINTENANCE REMOVED AND REPLACED HAT CHANNEL P/N 601R75262-159 IAW CRJ 200 SRM 51-42-06. (M)

Part: ANGLE — CRACKED (BS 625) · airframe 7,893 hrs · 8,615 cycles

LT OBLIQUE ANGLE AT STA 625 HAS .5 INCH CRACKED IN RADIUS. (K) MAINTENANCE INSTALLED NEW ANGLE CRJ SRM 51-42-06. (M)

Part: ANGLE — CRACKED (BS 625) · airframe 8,615 hrs · 7,906 cycles

RT OBLIQUE ANGLE AT STA 625.00 HAS A .5 INCH CRACKED IN RADIUS. (K) MAINTENANCE INSTALLED NEW ANGLE IAW CRJ SRM 51-42-06. (M)

Part: UNKNOWN — UNKNOWN (FLAP WARNING)

FLAPS FAIL CAUTION MESSAGE INFLIGHT AFTER FLAP 8 TAKEOFF AFTER FLAP RETRACTION ALT, MOVED FLAP HANDLE TO ZERO, FLAPS STAYED AT 8. AIRSPEED 170 KTS OAT 21 DEGREES C. PERFORMED FLAPS FAIL CHECKLIST AND FLAPS 8 LANDING. TOUCHDOWN 164 KTS AT 100/MIN. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4, FLAP SYSTEM RESET OK. AIRCRAFT GOOD FOR RETURN TO SERVICE. (M)

Part: UNKNOWN — UNKNOWN (FLAP WARNING)

FLAPS FAIL CAUTION MESSAGE AND FLAPS FAIL AT 0 DEGREES. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4, FLAPS RESET. AIRCRAFT RELEASED FOR SERVICE, NO SDU LIGHTS ILLUMINATED AT THIS TIME. (M)

Part: BRACKET — CRACKED (LT HYD SYS)

LEFT HYDRAULIC TRANSDUCER BRACKET, P/N 601R75262-159, CRACKED APPROXIMATELY .1 INCH LONG IN LEFT MLG WHEEL WELL CEILING. INSTALLED NEW BRACKET IAW CRJ SRM 51-42-06. (M)

Part: DOOR — OPEN (RT NACELLE)

PERFORMED AIR RETURN AFTER N1 FAN VIBRATION ON NR 2 ENGINE ASSOCIATED WITH AIRFRAME VIBRATION. VERTICAL DESCENT RATE LESS THAN 360 FPM AT TOUCHDOWN. LANDING WEIGHT 51,000 LBS. OVERWEIGHT LANDING INSPECTION NOT REQUIRED. RT ENGINE UPPER TRANSLATING COWL OPENED IN FLIGHT. REMOVED AND REINSTALLED ORIGINAL DAMAGED UPPER TRANSLATING COWL IAW CRJ AMM 71-11-01 AND REQUIRED REO FROM SHORTS FOR DAMAGE. COMPLIED WITH REQUIRED REO 601R-78-33-3528 REV WC20 FOR TAP TEST. APPLIED PAINT TO SCRATCH. APPLIED YELLOW DOT TO DENT. (M)

Part: FLAP — MALFUNCTIONED (WING) · airframe 7,647 hrs · 6,958 cycles

AFTER TAKEOFF WHILE RETRACTING FLAPS FROM 20 DEGREES. COMPLIED WITH QRH, FLAPS FAIL CAUTION MESSAGE ON ED1. COMPLIED WITH SUPPLEMENT 98-018A, NO FLAP TWISTING, SKEWING OR DEFORMATION NOTED. RESET CIRCUIT BREAKER ONCE, MESSAGE CLEARED, FLAPS OPERATE NORMALLY. (K)

Part: ELEMENT — MALFUNCTIONED

ANTI-ICE DUCT MESSAGE WITH DUCT FAIL IN SWITCH LIGHT WITH WING ANTI-ICE LIGHT ON. COMPLIED WITH QRH, SELECTED 14TH STAGE BLEEDS AND WING ANTI-ICE OFF. MESSAGE CLEARED. WHEN 14TH STAGE BLEEDS SELECTED ON AND WING ANTI-ICE TO STANDBY, MESSAGE DID NOT REAPPEAR. REMOVED AND REPLACED SENSING ELEMENT A47WK REF AMM 36-21-04, OPS CHECK GOOD. (M)

Part: SENSOR — FAILED (LT TE FLAP) · airframe 7,001 hrs · 6,311 cycles

MESSAGE DURING FLAP RETRACTION ON CLIMBOUT, FLAP FAIL AT ZERO. FOUND LT BRAKE POSITION SENSOR UNIT HARD FAILED. REPLACED BPSU IAW AMM 27-51-10. FLAPS CHECK GOOD. (K)

Part: CARBON SEAL — LEAKING (RT ENGINE)

RT ENGINE OIL LOW PRESSURE ILLUMINATED EN ROUTE, WITH THROTTLE RETARDED, OIL PRESSURE DROPPED FROM 48 TO 28 PSI. ENGINE WAS SHUTDOWN MANUALLY. PERFORMED ENGINE OIL CONSUMPTION CHECK PER AWAC SUPPLEMENT 06-025. FOUND STARTER CARBON SEAL LEAKING. REMOVED AND REPLACED STARTER CARBON SEAL ERF AMM 72-60-00. OPS CHECK GOOD. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

FIRST OFFICERS FRONT WINDSCREEN SHATTERED, CRACKED AFTER TAKEOFF AND SHATTERED PRIOR TO 4000 FEET. HEAT WAS SELECTED ON. REMOVED AND REPLACED FIRST OFFICERS RT WINDSHIELD. OPS CHECK GOOD. (M)

Part: SKIN — LIGHTNING STRIKE (FS 654) · airframe 3,714 hrs · 3,212 cycles

FUSELAGE SKIN HAS SUSTAINED LIGHTNING STRIKE DAMAGE AT FS 654.5 BETWEEN STR 26R AND 27R. REPAIRED DAMAGED AREA BY INSTALLING AN EXTERNAL DOUBLER AT FS 654.5 BETWEEN STR 26R AND 27R IAW EO AND SRM. (K)

Part: SKIN — CRACKED (PAX DOOR)

PASSENGER DOOR AFT SKIN DAMAGED AND INTERNAL STIFFENER CRACKED BELOW SKIN RIGHT STIFFENER CRACKED COMPLETELY IN HALF 1.5 INCH. INSTALLED REPAIR FILLER AND DOUBLE IAW BRAS EO 601R-52-7054A. (M)

Part: SUPPORT BEAM — CRACKED (CARGO DOOR)

CARGO DOOR SUPPORT BEAM MEMBER ANGLE, P/N 601R35050-109, CRACKED AT PRESSURE BULKHEAD FS 621, LBL 34.42. FABRICATED NEW CARGO DOOR SUPPORT BEAM ANGLE IAW CRJ200 SRM 51-30-06 AND BOMBARDIER DRAWING NR 601R35050, INSTALLED ANGLE IAW CRJ200SRM 51-42-21. (M)

Part: DOOR — OPEN (GROUND SERVICE)

DURING CLIMB-OUT, EXPERIENCED EXTREMELY LOUD NOISE FROM NOSE OF AIRCRAFT. RETURN TO FIELD. FOUND GROUND SERVICE DOOR OPEN. INSPECTED AND NO DAMAGE NOTED. CLOSED AND SECURED DOOR. NO FURTHER OCCURRENCES OR DEFECTS. (M)