N433AW

Part: BALLAST — SMOKE · airframe 47,465 hrs · 46,085 cycles

DISCREPANCY: CREW WITNESSED SMOKE COMING FROM ABOVE BIN OVER ROW 10AB AS WELL AS BURN MARKS ON THE CEILING. ****AIRCRAFT REMOVED FROM SERVICE***** REMOVED AND REPLACED SIDEWALL BALLAST LOCATED AT 10AB. OPS CHECK GOOD. IAW AMM 33-21-10. REF 339930-2 FOR BURN MARKS ON CEILING AND INSULATION.

Part: NONE — GOUGED · airframe 46,956 hrs · 45,610 cycles

CARGO DOOR FWD ROLLER TRACK AT FS 574.00 AND STR 12L TO STR 13L HAS WEAR DAMAGE MEASURING .200"L X .200"W X .020"D (P1) ON UPPER SIDE AND .300"L X .200"W X .040"D (P2) ON LOWER SIDE. THE TRACK IS MACHINED FROM 7075-T7451 PLATE WITH A LOCAL FLANGE THICKNESS OF 0.165". **************AIRCRAFT REMOVED FROM SERVICE************************* BLENDED BOTH AREAS SMOOTH AT (P1) .200"L X .200"W X .020"D AND AT (P2) .300"L X .200"W X .040"D AT WEAR AREAS ON FWD TRACK IAW ASAP EA #AWAC-CRJ253-01812 REV A DATED 03-08-2022. HFEC INSPECTION PERFORMED AT ALL BLEND AREAS IAW CRJ200 NDT MANUAL PART 1 51-20-06 REV 43. ROTO-PEENED REWORK AREAS AT (P1) AND (P2) IAW CRJ200 SRM 51-24-11 REV 38. RESTORED PROTECTIVE FINISH AT ALL REWORK AREAS IAW CRJ200 SRM 51-21-16 REV 38. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01812 REV A DATED 03/08/2022. WORK COMPLETED ON AERSALEWO #003566 CARD #20199 AT AERSALE CRS #4AER685B. N433AW TT:46,956:36 TC:45,610

Part: NONE — CORRODED (FS559+80-559+115) · corrosion level 2 · airframe 46,956 hrs · 45,610 cycles

R/H O/B FLOOR SILL AT FS 559+80 TO FS 559+115 AND LATERAL FLOOR BEAM AT 559+80 I/B AFT CORNER ARE CORRODED. CLEANED I/B LATERAL FLOOR BEAM AT FS 559+80 IAW CRJ200 51-26-00 REV 38. UPON FURTHER INVESTIGATION OF I/B LATERAL FLOOR BEAM AT FS 559+80 FOUND NO CORROSION ON BEAM. BLENDED 8 EACH AREAS ON R/H FLOOR SILL AT FS 559+80 TO FS 559+115 AND RBL 41 IAW BOMBARDIER GREO #601R53-00-526 REV (--) DATED 05-22-2013. R/H O/B FLOOR SILL AT FS 559+80 TO FS 559+115 AND RBL 41 BLENDED AREAS ARE NOT WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO #601R53-00-526 REV (--) DATED 05-22-2013. ***********AIRCRAFT REMOVED FROM SERVICE***************************** REMOVED AND REPLACED R/H O/B FLOOR SILL AT FS 559+80 TO FS 559+115 AND RBL 41 IAW CRJ200 SRM 51-42-00 REV 38 AND CRJ200 SRM 51-42-06 REV 38. RESTORED PROTECTIVE/DECORATIVE FINISH AT R/H O/B FLOOR SILL FS 559+80 TO FS 559+115 AT RBL 41 AND LATERAL FLOOR BEAM AT FS 559+80 I/B CORNER IAW CRJ200 SRM 51-25-06 REV 38. WORK ACCOMPLISHED ON AERSALE WO #003566 CARD #20264 AT AERSALE CRS #4AER685B TT:46,956:36 TC:45,610 N433AW

Part: NONE — CORRODED (FS349 - FS409+12) · corrosion level 2 · airframe 46,956 hrs · 45,610 cycles

R/H SIDEWALL SEAT TRACKS FROM FS 349.00 TO FS 409+128 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS349 TO FS 409+16 AT RBL 42 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38. R/H SEAT TRACK AT FS409+16 TO FS409+128 EVALUATED AND FOUND NO CORROSION AT THIS TIME. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH SIDEWALL SEAT TRACK FROM FS349 TO FS409+16, AND REINSTALLED SEAT TRACK FROM FS 409+16 TO FS 409+128 AT RBL 42 IAW IAW CRJ200 AMM 53-01-11 REV 64. RESTORED PROTECTIVE FINISH TO 2 EACH SEAT TRACK INSTALLATIONS PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 38, CRJ200 SRM 51-25-06 REV 38, AND CRJ200 SRM 51-25-00 REV 38. WORK COMPLETED ON AERSALE WO #003566 CARD #20071. CRS #4AER685B N433AW TT:46,956:36 TC:45,610

Part: NONE — CORRODED (FS409+111.98-559) · corrosion level 2 · airframe 46,956 hrs · 45,610 cycles

R/H SIDEWALL SEAT TRACKS FROM FS 409+111.98 TO FS 559+79 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS409+111.98 TO FS 559.00+79 AT RBL 42 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 4 EACH SIDEWALL SEAT TRACKS FROM FS409+111.98 TO FS458.06, FS458.06 TO FS510, FS510 TO FS549.06, FS549.06 TO FS 559+79 AT RBL 42 IAW IAW CRJ200 AMM 53-01-11 REV 64. RESTORED PROTECTIVE FINISH TO 4 EACH SEAT TRACK INSTALLATIONS PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 38, CRJ200 SRM 51-25-06 REV 38, AND CRJ200 SRM 51-25-00 REV 38. WORK COMPLETED ON AERSALE WO #003566 CARD #20073. CRS #4AER685B N433AW TT:46,956:36 TC:45,610

Part: NONE — CRACKED (FS 621) · airframe 46,956 hrs · 45,610 cycles

L/H CABIN FLOOR SUPPORT ANGLE P/N: 601R 53-61-004-1 HAS A CRACK .900"L ON FORWARD INBOARD END. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED PREVIOUS REPAIR SPLICE ON L/H CABIN FLOOR SUPPORT ANGLE P/N: 601R-53-61-004-1 (13.3"L X 2.7"W) IAW BOMBARDIER REO 601R 53-61-117 REV E DATED 2018-01-15 22 HFEC INSPECTION PERFORMED AT CUT AREAS WITH NO INDICATIONS IAW CRJ200 NDT MANUAL PART 1 51-20-06 REV 43. RESTORED PROTECTIVE FINISH AT REPAIR AREA IAW CRJ200 SRM 51-25-06 REV 38. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW BOMBARDIER REO 601R-53-61-117 REV E DATED 2018-01-15. WORK COMPLETED ON AERSALE WO #003566 CARD #20261. CRS #4AER685B N433AW TT:46,956:36 TC:45,610

Part: NONE — CORRODED (AFT LAV SERVICE) · corrosion level 2 · airframe 46,956 hrs · 45,610 cycles

AFT LAVATORY SERVICE DOOR LOWER HINGE HAS CORROSION. REMOVED CORROSION AT AFT LAVATORY SERVICE DOOR LOWER HINGE BRACKET IAW CRJ200 SRM 51-12-00 REV 38. EVALUATED CORROSION REMOVAL ON AFT LAVATORY SERVICE DOOR HINGE BRACKET AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-51-26 REV 38. ***********AIRCRAFT REMOVED FROM SERVICE***************************** REMOVED LOWER HINGE BRACKET AT AFT LAVATORY SERVICE DOOR IAW CRJ200 SRM 51-42-20 REV 38. FABRICATED I/B HINGE BRACKET AT AFT LAVATORY SERVICE DOOR LOWER HINGE OUT OF 7075-T62 .063" MATERIAL IAW CRJ200 SRM 53-51-26 REV 38 AND CRJ200 SRM 51-12- 00. INSTALLED FABRICATED HINGE BRACKET AT AFT LAVATORY SERVICE DOOR LOWER HINGE IAW CRJ200 SRM 51-42-20 REV 38. WORK ACCOMPLISHED ON AERSALE WO #003566 CARD #20048 AT AERSALE CRS #4AER685B TT:46,956:36 TC:45,610 N433AW

Part: NONE — CORRODED (FS 364 TO FS 394) · corrosion level 2 · airframe 46,956 hrs · 45,610 cycles

R/H FLOOR SEAT TRACK FROM FS 364TO FS 394 AND RBL 9 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS 364 TO FS 394 AT RBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 38. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED CABIN FLOOR SEAT TRACK FROM FS 364 TO FS 394 AND RBL 9, IAW CRJ200 AMM 53-01-11 REV 64. RESTORED PROTECTIVE FINISH TO SEAT TRACK INSTALLATION PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 38, CRJ200 SRM 51-25-06 REV 38, AND CRJ200 SRM 51-25-00 REV 38. WORK COMPLETED ON AERSALE WO #003566 CARD #20241. CRS #4AER685B N433AW TT:46,956:36 TC:45,610

Part: FITTING — CORRODED (FS 341 TO FS 345) · corrosion level 2 · airframe 46,956 hrs · 45,610 cycles

CORROSION ON PASSENGER DOOR FITTING P/N: 601R31527-217 AT FS 341 TO FS 345 AND LBL 42 TO LBL 44 AND WL 73.50. ************AIRCRAFT REMOVED FROM SERVICE**************************** UPON FURTHER INSPECTION, FOUND SEVERE CORROSION ON PASSENGER DOOR BRACKET P/N: 601R31527-217 IAW CRJ200 SRM 51-11-00 REV 38. REMOVED AND REPLACED PASSENGER DOOR BRACKET P/N: 601R31527-217 IAW CRJ200 SRM 51-42-06 REV 38. RESTORED CIC PROTECTION IAW CRJ200 SRM 51-21-11 REV 38. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW CRJ 200 SRM 51-42-06 REV 38. WORK COMPLETED ON AERSALE WO #003566 CARD #20115 AT AERSALE CRS #4AER685B.

Part: NONE — CORRODED (FS574-FS621) · corrosion level 2 · airframe 46,956 hrs · 45,610 cycles

L/H CABIN FLOOR LANDING PLATE P/N: 601R35011-63 HAS AREA OF SURFACE CORROSION AT FS 574 TO FS 621 AT LBL 42 TO LBL 46. *********AIRCRAFT REMOVED FROM SERVICE*************************** BLENDED AREA ON L/H CABIN FLOOR LANDING PLATE P/N: 601R35011-63 AT FS 574 TO FS 605 AT LBL 43 WITH AN ORIGINAL THICKNESS OF .050" AND A REMAINING THICKNESS OF .040" AND FOUND WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R 53-00-526 REV (--) DATED 22 MAY 2013. BLENDED AREA ON L/H CABIN FLOOR LANDING PLATE P/N: 601R35011-63 AT FS 605 TO FS 621 AT LBL 43 WITH AN ORIGINAL THICKNESS OF .050" AND A REMAINING THICKNESS OF .037" AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW BOMBARDIER GREO 601R 53-00-526 REV (--) DATED 22 MAY 2013. RE-EVALUATED BLEND AREA ON L/H CABIN FLOOR LANDING PLATE P/N: 601R35011-63 AT FS 605 TO FS 621 LBL 43 AND FOUND WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01824 REV IR DATED 03/15/2022. HFEC INSPECTION PERFORMED AT BLEND AREAS WITH NO INDICATIONS IAW CRJ200 NDT MANUAL PART 1 51-20-06 REV 43. RESTORED PROTECTIVE FINISH AT REPAIR AREA IAW CRJ200 SRM 51-25-06 REV 38. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01824 REV IR DATED 03/15/2022. WORK COMPLETED ON AERSALE WO #003566 CARD #20261. CRS #4AER685B N433AW TT:46,956:36 TC:45,610

Part: NONE — DENTED (FS 625 TO FS 640) · airframe 46,956 hrs · 45,610 cycles

AIRCRAFT L/H SKIN EXTERIOR HAS 2 EACH DENTS AT FS 625 TO FS 640 AND S19L TO S20L. DENT DIMENSIONS ARE: (P1) 1.0"L X .900"W X .015"D; (P2) .800"L X .800"W X .012"D. EVALUATED BOTH DENTS AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE*********************** VERIFIED NO LOOSE/PULLED FASTENERS AND NO DAMAGE TO UNDERLYING STRUCTURE COMMON TO (P1) & (P2) AREAS. HFEC PERFORMED WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. RE-EVALUATED SKIN AND FOUND WITHIN LIMITS IAW ASAP EA # AWAC-CRJ253-01821 REV IR DATED 03/11/2022. ALL WORK PERFORMED IAW ASAP EA #AWAC-CRJ253-01821 REV IR DATED 03/11/2022. WORK COMPLETED AT AERSALE CRS#4AER685B ON W/O #003566 CARD #20202. N433AW TT:46,956:36 TC: 45,610

Part: NONE — CORRODED (FS 364 TO FS 394) · corrosion level 2 · airframe 46,956 hrs · 45,610 cycles

R/H FLOOR SEAT TRACK FROM FS 364TO FS 394 AND RBL 9 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACKS AT FS 364 TO FS 394 AT RBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 38. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED CABIN FLOOR SEAT TRACK FROM FS 364 TO FS 394 AND RBL 9, IAW CRJ200 AMM 53-01-11 REV 64. RESTORED PROTECTIVE FINISH TO SEAT TRACK INSTALLATION PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 38, CRJ200 SRM 51-25-06 REV 38, AND CRJ200 SRM 51-25-00 REV 38. WORK COMPLETED ON AERSALE WO #003566 CARD #20241. CRS #4AER685B N433AW TT:46,956:36 TC:45,610

Part: NONE — CORRODED (FS589 TO FS 621) · corrosion level 2 · airframe 46,956 hrs · 45,610 cycles

L/H CABIN FLOOR SUPPORT BEAM P/N: 601R35031-3 HAS CORROSION AT FS 589 TO FS 621 AND LBL 27. *********AIRCRAFT REMOVED FROM SERVICE*************************** BLENDED AREA OF CORROSION ON FLOOR SUPPORT BEAM P/N: 601R35031-3 AT FS 589-621 WITH ORIGINAL MATERIAL THICKNESS .050" AND A REMAINING THICKNESS OF .027" AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-61-43 REV 38 & SRM 53-00-00 REV 38. REMOVED AND REPLACED L/H CABIN FLOOR SUPPORT BEAM FS 589 TO FS 621 LBL 27 P/N: 601R35031-3 IAW CRJ200 SRM 51-42-21 REV 38. RESTORED PROTECTIVE FINISH AT REPAIR AREA IAW CRJ200 SRM 51-25-06 REV 38. WORK COMPLETED ON AERSALE WO #003566 CARD #20261. CRS #4AER685B N433AW TT:46,956:36 TC:45,610

Part: NONE — CORRODED (FS409+111.98-559) · corrosion level 2 · airframe 46,956 hrs · 45,610 cycles

L/H SIDEWALL SEAT TRACKS FROM FS 409+111.98 TO FS 559+79 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON L/H SIDEWALL SEAT TRACKS AT FS409+111.98 TO FS 559.00+79 AT RBL 42 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 4 EACH SIDEWALL SEAT TRACKS FROM FS409+111.98 TO FS458.06, FS458.06 TO FS510, FS510 TO FS549.06, FS549.06 TO FS 559+79 AT LBL 42 IAW IAW CRJ200 AMM 53-01-11 REV 64. RESTORED PROTECTIVE FINISH TO 4 EACH SEAT TRACK INSTALLATIONS PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 38, CRJ200 SRM 51-25-06 REV 38, AND CRJ200 SRM 51-25-00 REV 38. WORK COMPLETED ON AERSALE WO #003566 CARD #20074. CRS #4AER685B N433AW TT:46,956:36 TC:45,610

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 46,587 hrs · 45,239 cycles

CLIMBING THRU FLIGHT LEVEL 180 RECEIVED FLAP FAIL MSG CW QRH LANDED AT FLAP ZERO DEG. SMOOTH LANDING MAX BTMS 4. PERFORMED FLAP RESET PROCEEDURE IAW AWAC SUP 98-018I BOX 12 FLAPS RESET. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT PER AMM 27-51-05 OPS CHECK GOOD.

Part: WATER SEPARATOR — ODOR (RIGHT) · airframe 46,427 hrs · 45,069 cycles

HAZE/SMOKE IN CABIN ON INSPECTION RT PACK 120C. UNABLE TO COOL IN MANUAL OR AUTO MODE. LT PACK IS OPERATING NORMALLY. BOTH PACKS WERE RUNNING OFF OF APU AIR. ***AIRCRAFT REMOVED FROM SERVICE*** REF WO 310433 WC 3,4,5 FOR R&R OF LH ACM IN COMPLIANCE OF AWA SUP 09-037D OPS CHECKS GOOD

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 45,490 hrs · 44,056 cycles

FLAPS FAILED AT ZERO IN CRUISE. ALT 14K FT PERFORMED QRH UNEVENTFUL LANDING. PERFORMED FLAP RESET PROCEEDURE, IAW AWAC SUP 98-18I BOX 12 FLAPS RESET. PLACRDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT FLAP BPSU, PER AMM 27-51-10. OPERATIONS CHECK GOOD. REMOVED FROM MEL. REMOVED PLACARD.

Part: CONTROL CABLE — DAMAGED (LT AILERON) · airframe 44,688 hrs · 43,214 cycles

OUTBOARD FUSELAGE AILERON CIRCUIT CABLE FOUND DAMAGED AT QUADRANT. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED LEFT HAND OUTBOARD FUSELAGE CABLE REF. CRJ-200 AMM 27-00-00 AND 27-11-00 REV. 60

Part: SKIN — DAMAGED (LT WING) · airframe 44,688 hrs · 43,214 cycles

L/H WING LWR AFT PLANK I/B OF FWD FITTING @ WS 178.00 HAS A SCRATCH INTO METAL. AIRCRAFT REMOVED FROM SERVICE BLENDED SCRATCH ON L/H WING LWR AFT PLANK I/B OF FWD FITTING @ WS 178.00 BLEND MEASUREMENTS ARE 1.0"L X .040"W X .006"D, NO CRACKS NOTED AT THIS TIME WITHIN ALLOWABLE LIMITS REF BOMBARDIER REO 601-57-21-3250 REV A DTD 2020-02-01.

Part: CONTROL CABLE — DAMAGED (RT AILERON) · airframe 44,688 hrs · 43,214 cycles

RIGHT HAND OUTBOARD AILERON FUSELAGE CABLE FRAYED AT RIGHT HAND QUADRANT. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED RIGHT HAND OUTBOARD AILERON FUSELAGE CABLE REF. CRJ-200 AMM 27-11-00 REV. 60

Part: FITTING — GOUGED (BS 473) · airframe 44,688 hrs · 43,214 cycles

L/H WING AFT WING TO FUSELAGE FITTINGS (UPPER & LOWER) HAVE TOOLING MARKS. AIRCRAFT REMOVED FROM SERVICE BLENDED DAMAGE TO SMOOTH CONTOUR ON THE L/H WINGBOX TO FUSELAGE MACHINED FRAME AT FS 473.15 BLEND DIMENSIONS FOUND TO BE .500"L X .200"W X .043"D, NDT PERFORMED WITH NO DEFECTS NOTED AT THIS TIME, AND IS WITHIN ALLOWABLE LIMITS. REF CRJ-200 SRM 51-41-15 AND SRM 53-00-00. BLENDED DAMAGE TO SMOOTH CONTOUR ON THE L/H WINGBOX TO FUSELAGE FITTING AT FS 473.15 BLEND DIMENSIONS FOUND TO BE .850"L X .215"W X .027"D, NDT PERFORMED WITH NO DEFECTS NOTED AT THIS TIME, AND IS STRUCTURALLY ACCEPTABLE REF BOMBARDIER REO 601R-57-21-3253 DTD 2020-02-07.

Part: HINGE — GOUGED (PAX DOOR) · airframe 44,688 hrs · 43,214 cycles

ENTRY DOOR HINGE ON DOOR SIDE HAS MULTIPLE LUGS WITH WEAR. AIRCRAFT REMOVED FROM SERVICE LUG #26 BLENDED BELOW .100" LIMIT REFERENCE REO REF REO 601R-52-11-1347 REV C DTD 2017-08-02. DOOR HINGE LUG BLENDED TO .094" PERFORMED A SMOOTH CONTOUR OF 5:1 PERFORMED NDT WITH NO CRACK INDICATIONS AT THIS TIME AND FOLLOWED ALL OTHER REQUIREMENTS OF GENERIC REO 601R-52-11-1347 REV C ARE MET, AND IS CONSIDERED STRUCTURALLY ACCEPTABLE REF REO 601R-52-11-2792 DTD 2020-02-05

Part: PRESSURE SWITCH — MALFUNCTIONED (LT WING ANTI-ICE) · airframe 44,378 hrs · 42,917 cycles

3158 - L WING ANTI ICE CAUTION MESSAGE IN FLIGHT. C/W QRH MESSAGE CLEARED AND LEFT ICING CONDITIONS MESSAGE OCCURED BETWEEN CLIMBOUT AND CRUISE WITH WING ANTI ICE SELECTED ON. L WING SHOWED YELLOW ON SYNOPTIC MESSAGE CLEARED WHEN 14TH STAGE ISOL VALVE OPENED AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED LH PRESSURE SW IAW AMM 30-12-10. OPS CHECK GOOD

Part: LANDING GEAR — MALFUNCTIONED · airframe 43,929 hrs · 42,475 cycles

AFTER TAKE-OFF, RECEIVED WARNING FOR GEAR DISAGREE. NOSE WHEEL WAS SHOWING YELLOW BOX, THEN UP 2 TIMES. ON EXTENSION, NOSE GEAR TOOK LONGER TO EXTEND WITH EXTRA NOISES FROM GEAR DURING EXTENSION. HYDRAULIC SYSTEMS SHOW NORMAL. CREW REPORTED VIA ACARS THAT THEY EXPERIENCED A NOSE WHEEL GEAR DISAGREE AFTER TAKEOFF. DID NOT DECLARE AN EMERGENCY AND RETURNED TO DEPARTURE FOR AN UNEVENTFUL LANDING AND WERE ABLE TO TAXI BACK TO A GATE ON THEIR OWN.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSER) · airframe 43,832 hrs · 42,385 cycles

R TR UNLOCK (C) IN FLIGHT AT 29,000FT 290 KT AMBER REV ICON. T/R APPEARS PHYSICALLY STOWED. EMER STOW PRESSED MSG REMAINED. DURING THE CRUISE, THE FLIGHT CREW RECEIVED A THRUST REVERSER UNLOCKED CAUTION MESSAGE. AFTER COORDINATING WITH DISPATCH AND WORKING THROUGH THE QRH, THE FLIGHT WILL DIVERT TO BUF.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 43,390 hrs · 41,964 cycles

4804 RT REV UNLCKEDE CAUTION MSG ILLUMINATED IN FLT. CW QRH MSG DID NOT CLEAR. DIVERTED TO DAY. REV ICON IN RT N1 IND. MSGS CLEARED ON ENGINE SHUTDOWN. RT TR APPEARS TO BE STOWED.

Part: PSEU — FAULTED (MLG) · airframe 41,411 hrs · 40,021 cycles

DURING CRUISE, RECEIVED A PROXIMITY SYS CHANNEL CAUTION MESSAGE. COMPLIED WITH QRH. MANUAL GEAR EXTENSION, NWS SELECTED OFF, LANDED WITHOUT ISSUE, TOWED OFF RUNWAY TO THE GATE. PSEU FAULTED, REPLACE PSEU

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 41,132 hrs · 39,712 cycles

FRAMES 333 BETWEEN STR'S 25R AND 25L CORRODED. REPLACED

Part: FRAME — CORRODED (BS 349) · corrosion level 2 · airframe 41,132 hrs · 39,712 cycles

E&E BAY FRAME BS 349, STRINER 25L TO 25R CORRODED. REPLACED THE FRAME.

Part: STRUCTURE — DENTED (BS 589-604) · airframe 41,132 hrs · 39,712 cycles

STRUCTURE DENTED BETWEEN BS 589 AND 604. REPAIRED THE STRUCTURE.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 41,132 hrs · 39,712 cycles

MAIN CABIN LEFT FLOOR SUPPORT IN PAX DOOR CORRODED. REPLACED THE FLOOR SUPPORT

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 41,132 hrs · 39,712 cycles

LEFT INBD FLAP VANE IS CHAFED ON THE LE IN MULTIPLE AREAS. REPLACED THE FLAP VANE

Part: ATTACH FITTING — CRACKED (NR 1 PYLON) · airframe 41,132 hrs · 39,712 cycles

NR 1 PYLON LE ACCESS ATTACH FLANGE IS CRACKED ON THE LOWER PYLON.

Part: RIB — DAMAGED (LT WING TE FLAP) · airframe 41,132 hrs · 39,712 cycles

ON REMOVAL OF THE LT WING FLAP VANE INBD LE, FOUND DAMAGED FASTENER HOLES IN THE INBD RIB. REPLACED THE RIB.

Part: FRAME — CRACKED (BS 605) · airframe 41,132 hrs · 39,712 cycles

FRAME AT BS 605 ATTACH FLANGES CRACKED JUST ABOVE AND BELOW STRINGER 9L. REPAIRED THE FRAME.

Part: FLOOR SUPPORT — CORRODED (BS 349-409) · corrosion level 2 · airframe 41,132 hrs · 39,712 cycles

LEFT CABIN FLOOR SUPPORT BS 349 - 409, LBL 42-46 CORRODED. REPAIRED THE FLOOR SUPPORT

Part: INTERCOSTAL — CORRODED (BS 320-338) · corrosion level 2 · airframe 41,132 hrs · 39,712 cycles

PAX DOOR INTERCOSTAL DD 7 CORRODED. REPLACED THE INTERCOSTAL.

Part: SKIN — CRACKED (BS 169-193) · airframe 41,132 hrs · 39,712 cycles

CRACKED SKIN ON THE LT LOWER NOSE HYD COMPARTMENT AFT UPPER LATCH CUT OUT.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 41,132 hrs · 39,712 cycles

RIGHT INBD FLAP LOWER SURFACE SKIN NICKED.

Part: STRUCTURE — CORRODED (BS 343) · corrosion level 2 · airframe 41,132 hrs · 39,712 cycles

MAIN CABIN, BS 343, LBL 39 HINGE CUTOUR IS CORRODED. REPLACED THE STRUCTURE.

Part: FRAME — CRACKED (BS 718) · airframe 41,132 hrs · 39,712 cycles

BS 718 FRAME FLANGE CRACKED. REPAIRED THE FRAME.

Part: STRUCTURE — CORRODED (BS 316) · corrosion level 2 · airframe 41,132 hrs · 39,712 cycles

MAIN CABIN, BS 316, LBL 39 HINGE CUTOUT IS CORRODED. REPLACED THE STRUCTURE.

Part: SKIN — CORRODED (LT WING TE FLAP) · airframe 41,132 hrs · 39,712 cycles

LEFT INBD FLAP INBD LOWER SKIN PANEL PITTED.

Part: FASTENER — MISSING (FLOOR SKIN) · airframe 41,132 hrs · 39,712 cycles

RIGHT UPPER PRESSURE FLOOR SKIN IS MISSING 7 RIVETS FROM BS 513 - 559 ON TOP OF RBL 36, IN THE CABIN.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 41,132 hrs · 39,712 cycles

BS 280 STRINGER 3L CRACKED. REPLACED THE STRINGER CLIP.

Part: ANGLE — CRACKED (HYDRAULIC BAY) · airframe 41,132 hrs · 39,712 cycles

LT LOWER NOSE (HYDRAULIC) COMPARTMENT HAS CRACKED ANGLE AT FS200 WL78 ABOVE HYDRAULIC COMPENSATOR.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,132 hrs · 39,712 cycles

LT PRESSURE FLOOR STRUCTURE ANGLE AT LBL43 IS CORRODED FROM FS409+128 TO FS559.

Part: POST — CRACKED · airframe 41,132 hrs · 39,712 cycles

VERTICAL POST AT LBL 18 IS CRACKED IN THE OTBD RADIUS. REPLACED.

Part: ANGLE — CRACKED (BS 621) · airframe 41,132 hrs · 39,712 cycles

CRACKED ANGLE ATTACHED TO THE AFT FACE OF BS 621 BULKHEAD OB OF LBL36 AT WL 83. REPLACED

Part: INTERCOSTAL — CORRODED (BS 349-364) · corrosion level 2 · airframe 41,132 hrs · 39,712 cycles

1015062 1000-0013 - FWD RH IB INTERCOSTAL BETWEEN FS 349 AND 364 AT STGR 27 CORRODED. REPLACED

Part: ANGLE — CRACKED (BS 484) · airframe 41,132 hrs · 39,712 cycles

1015062 1000-0072 - ANGLE CLIP AT THE OB SIDE OF RBL 9 AT FS 484 CRACKED. REPLACED

Part: ANGLE — CRACKED (BS 484) · airframe 41,132 hrs · 39,712 cycles

1015062 1000-0065 - ANGLE CLIP AT THE OB SIDE OF RBL 27 AT FS 484 CRACKED. REPLACED

Part: BRACKET — CRACKED (RWS 143) · airframe 41,132 hrs · 39,712 cycles

1015062 6000-0025 - RH FWD FACE WING SPAR OUTBD BRACKET CRACKED ON PICOLLO TUBE TRANSITION ELBOE @ WS 143. REPLACED

Part: SUPPORT BRACKET — CRACKED (BS 478) · airframe 41,132 hrs · 39,712 cycles

1015062 1000-0007 - LH OB LONGERON ABOVE WING STA 478 FAIRING SUPPORT BRACKET CRACKED. REPLACED

Part: BRACKET — CRACKED (BS 470) · airframe 41,132 hrs · 39,712 cycles

1015062 1000-0008 - LH OB LONGERON ABOVE WING STA 470 FAIRING SUPPORT BRACKET CRACKED. REPLACED

Part: BRACKET — CRACKED (BS 461) · airframe 41,132 hrs · 39,712 cycles

1015062 1000-0004 - RH OB LONGERON ABOVE WING STA 461 FAIRING SUPPORT BRACKET CRACKED. REPLACED

Part: BRACKET — CRACKED (BS 470) · airframe 41,132 hrs · 39,712 cycles

1015062 1000-0005 - RH OB LONGERON ABOVE WING STA 470 FAIRING SUPPORT BRACKET CRACKED. REPLACED

Part: BRACKET — CRACKED (BS 449) · airframe 41,132 hrs · 39,712 cycles

1015062 1000-0010 - LH OB LONGERON ABOVE WING (BL 45L) STA 449 (APPROX) HAS CRACKED FAIRING SUPPORT BRACKET. REPLACED

Part: BRACKET — CRACKED (BS 461) · airframe 41,132 hrs · 39,712 cycles

1015062 1000-0009 - LH OB LONGERON ABOVE WING (BL 45L) STA 461 FAIRING SUPPORT BRACKET CRACKED. REPLACED

Part: BRACKET — CRACKED (BS 449) · airframe 41,132 hrs · 39,712 cycles

1015062 1000-0003 - RH OB LONGERON ABOVE WING STA 449 FAIRING SUPPORT BRACKET CRACKED. REPLACED

Part: BRACKET — CRACKED (BS 478) · airframe 41,132 hrs · 39,712 cycles

1015062 1000-0006 - RH OB LONGERON ABOVE WING STA 478 FAIRING SUPPORT BRACKET CRACKED. REPLACED

Part: COALESCER BAG — ODOR (LT & RT) · airframe 40,890 hrs · 39,460 cycles

OILY FUMES FROM PACKS WHEN 10TH STAGE IS SUPPLIED BY APU. REMOVED AND REPLACED LEFT AND RIGHT COALESCER SOCKS IAW AMM 21-51, OPS CHECKED GOOD, NO ODORS NOTED AT THIS TIME.

Part: PUMP — FAILED (NR 2 HYD) · airframe 34,064 hrs · 33,459 cycles

DURING THE AFTER TAKEOFF CHECKLIST, CREW NOTICED HYD 2 PRESSURE AT 1900 PSI. PRESSURE REMAINED AT 1900 PSI FOR 15-20 MINUTES. PRESSURE THEN FELL TO 1800 PSI. RAN QRH FOR HYD 2 LOW PRESSURE. PRESSURE INCREASED TO 2800 PSI WITH QTY AT 85 PERCENT. PRESSURE & QTY REMAINED CONSISTENT FOR 5 - 10 MINUTES. HYD 2 B STARTED MAKING GROWLING NOISES AND QTY WENT TO 100 PERCENT AND PRESSURE WENT TO 0 PSI. COMPLIED WITH EDP 2 QRH. LANDED. BMTS 4433, EDP2 WAS AT 0 PSI FOR 30 MINUTES. REMOVED HYD SYS NR 2 PRESSRUE MANIFOLD FILTER BECAUSE DPI WAS POPPED. FILTER CONTAINS DEBRIS. REPLACED EDP NR 2 IAW AMM 29-11-01 AND COMPLIED WITH FILTER R & R SUPPLEMENT 06-029C. SYSTEM TESTED, LEAKED CHECKED GOOD. REPLACED ALL NR 2 HYDRAULIC SYSTEM FILTERS IAW SUP 06-029C.

Part: HANDLE — DIRTY (SERVICE DOOR) · airframe 32,463 hrs · 32,001 cycles

GALLEY SERVICE DOOR WILL NOT OPEN FROM OUTSIDE, OPENS NORMALLY FROM INSIDE. CLEANED AND LUBED SERVICE DOOR OUTER HANDLE AND R & R OUTER HANDLE SPRING IAW AMM 52-41-03. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (CARGO BAY) · airframe 32,104 hrs · 31,665 cycles

AT GATE RECEIVED CARGO SMOKE WARNING MESSAGE, AND CARGO BOTTLE LOW CAUTION MESSAGE. NO OBSERVED SMOKE IN CARGO COMPARTMENT. ON CALL, MAINTENANCE REPORTED BOTH BOTTLES EMPTY UPON INSPECTION.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,388 hrs · 36,223 cycles

OUTBOARD INTERCOSTAL AT STRINGER 16L & FS 625 IS CRACKED. REMOVED CRACKED INTERCOSTAL AT STRINGER 16L & FS 625, REPLACED WITH NEW INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 37,388 hrs · 36,223 cycles

PASSENGER DOOR FWD UPPER INTERCOSTAL, NEXT TO THE FWD PULL IN LEVER TORQUE TUBE IS CRACKED, REPAIRED.

Part: SKIN — CRACKED (PAX DOOR) · airframe 37,388 hrs · 36,223 cycles

PASSENGER DOOR INNER SKIN FOUND CRACKED, AFT UPPER INNER SKIN. REPAIRED PAX DOOR INNER SKIN, AFT UPPER INNER SKIN IAW EA 30-2016-029 DATED 1 18 2016.

Part: STRUCTURE — CRACKED (RT WING) · airframe 37,388 hrs · 36,223 cycles

RIGHT WING, INBD LE UPPER AFT EDGE, CRACKED ABOVE PANEL 620AZ. REPAIRED RT WING, INBD LE UPPER AFT EDGE AT PANEL 620AZ IAW SUPPLEMENT 16-019 DATED 01 20 2016.

Part: SKIN — CRACKED (PAX DOOR) · airframe 37,388 hrs · 36,223 cycles

PASSENGER DOOR INNER SKIN, UNDER PANEL 832AL CRACKED, REPAIRED.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 37,388 hrs · 36,223 cycles

CARGO DOOR AFT LOWER INTERCOSTAL CRACKED, FS 605.00. REPLACED CARGO DOOR AFT LOWER INTERCOSTAL IAW SRM 51-42-06 & 51-42-10.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 37,388 hrs · 36,223 cycles

UPPER INTERCOSTAL UNDER PAX DOOR PANEL 832BR IS CRACKED, REPLACED.

Part: HOUSING — GOUGED (SERVICE DOOR) · airframe 37,388 hrs · 36,223 cycles

SERVICE DOOR OUTER HANDLE HOUSING INNER DIAMETER IS SCRATCHED & GOUGED, REPLACED.

Part: TEE FITTING — CRACKED (CARGO DOOR) · airframe 37,388 hrs · 36,223 cycles

CARGO DOOR LOWER VERTICAL INTERCOSTAL ATTACHING T IS CRACKED, FS 589.00. REPAIRED CARGO DOOR LOWER VERTICAL INTERCOSTAL ATTACHING T FITTING IAW EA 26-2016-014.

Part: WEB — CRACKED (FUSELAGE) · airframe 37,388 hrs · 36,223 cycles

UPPER AVIONICS FLOOR WEB CRACKED, LT SIDE AT FS 193. REPAIRED UPPER AVIONICS FLOOR WEB LT SIDE AT FS 193.00 IAW REO 601R-53-11-081.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,388 hrs · 36,223 cycles

OUTBOARD INTERCOSTAL AT FS 625.00 & STRINGER 15L IS CRACKED. REMOVED CRACKED INTERCOSTAL & REPLACED WITH NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,388 hrs · 36,223 cycles

OUTBOARD INTERCOSTAL AT STRINGER 13L & FS 625.00 IS CRACKED. REMOVED CRACKED INTERCOSTAL AT STRINGER 13L & FS 625.00. REPLACED WITH NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 37,388 hrs · 36,223 cycles

OUTBOARD INTERCOSTAL, STRINGER 14 L & FS 625 IS CRACKED. REMOVED CRACKED INTERCOSTAL AT STRINGER 14L & REPLACED WITH NEW SERVICEABLE PN 601R-35012-23 IAW SRM 51-42-06 & 51-42-21.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 37,388 hrs · 36,223 cycles

FLIGHT DECK, COPILOTS WINDOW POST AFT LOWER ATTACH FITTING CRACKED. R & R CRACKED ATTACH FITTING AT COPILOTS WINDOW POST AFT LOWER SIDE WITH NEW SERVICEABLE FITTING YAW SUM 51-42-21 & 51-40-11.

Part: WEB — CRACKED (FUSELAGE) · airframe 37,388 hrs · 36,223 cycles

UPPER AVIONICS FLOOR WEB CRACKED RT SIDE AT FS 193.00. REPAIRED UPPER AVIONICS FLOOR WEB AT RT FS 193.00 IAW REO 601R-53-11-245 REV B.

Part: FITTING — CRACKED (FUSELAGE) · airframe 37,388 hrs · 36,223 cycles

FS 484.00 CLIP LBL 27 IS CRACKED. R & R CLIP AT FS 484.00, LBL27 IAW REO 601R-53-41-059 REV B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,388 hrs · 36,223 cycles

RIGHT SIDE WALL SEAT TRACK NR 2 CORRODED, BETWEEN FS 409+16 - FS 409+112. R & R RT SIDE WALL SEAT TRACK NR 2 IAW AMM 53-01-11 & REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,388 hrs · 36,223 cycles

RIGHT AISLE SEAT TRACK STICK NR 1 HAS CORROSION, BETWEEN FS 364.00 & 394.00 IN THE CABIN. R & R SEAT TRACK NR 1 IAW AMM 53-01-11 & REO 601R-53-00-485.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 37,388 hrs · 36,223 cycles

LEFT WING LE CTR SECTION ATTACH ANGLE LOWER CORNER CRACKED. R & R LT WING LE CTR SECTION ATTACH ANGLE IAW SRM 51-41-02.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 37,388 hrs · 36,223 cycles

CARGO TIE DOWN TRACK, LBL 9, FS 559.00+90 HAS CORROSION. FABRICATED NEW CARGO TIE DOWN TRACK AT FS F59.00+90 & LBL 9 IAW REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,388 hrs · 36,223 cycles

RIGHT SIDE WALL SEAT TRACK NR 5 HAS CORROSION, BETWEEN FS 499 - FS 544 IN THE CABIN. R & R RT SIDE WALL SEAT TRACK NR 5 IAW AMM 53-01-11 & REO 601R-53-00-485.

Part: FITTING — CRACKED (BS 461) · airframe 37,388 hrs · 36,223 cycles

BATH TUB FITTING AT BS 461 LBL9 IS CRACKED. REMOVED AND REPLACED BATH TUB FITTING IAW SRM 51-42-21.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 37,388 hrs · 36,223 cycles

CARGO TIE DOWN TRACK LBL 9, FS 559+112, HAS CORROSION.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 37,388 hrs · 36,223 cycles

CARGO TIE DOWN TRACK LBL 9, FS 621, HAS CORROSION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,033 hrs · 30,657 cycles

FLOOR LEVEL EMER LIGHTS STARTING AT ROW 9 & AFT NOT ILLUMINATING.

Part: MODULE — MALFUNCTIONED (CABIN) · airframe 29,317 hrs · 28,989 cycles

WORK ORDER 222502 & 256327 112,113,114. 112 POSITIONS 3, 4, 7 & 8 OXYGEN MODULES ON THE A SIDE DID NOT DROP O2 MASKS DURING TEST. 113 SEAT ROWS 3A, 4A ,7A & 8A OXYGEN MODULES NEED INSTALLATION. OPERATIONS CHECKS. REF MX WC 12. 114 LAVATORY O2 MODULE DOOR LATCH WILL NOT STAY ENGAGED.

Part: LINE — BROKEN (HYD SYSTEM) · airframe 29,157 hrs · 28,841 cycles

HYDRAULIC SYS NR 2 QTY DROPPED TO 5 PERCENT. HYD SYS 2 SHOWS ZERO QTY & VARIABLE PRESSURE WITH 2B PUMP TURNED ON IN GATE. R & R BROKEN HYD LINE IN RT WW IAW 20-22-01. SERVICED NR 2 HYD SYS IAW AMM 12-12-29. OPERATIONS & LEAK CHECK OF HYD SYS 2 GOOD AT THIS TIME IAW AMM 29-10-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,109 hrs · 28,795 cycles

FORWARD EMERGENCY LIGHT AT AIR STAIR INOPERATIVE.

Part: TRIM SYSTEM — DISENGAGED (HORIZ STAB) · airframe 28,808 hrs · 28,526 cycles

STAB TRIM DISENGAGED MULTIPLE TIMES IN FLIGHT. MACH TRIM MSGS RECEIVED.

Part: WIRE HARNESS — KINKED (PAX DOOR) · airframe 33,785 hrs · 32,814 cycles

PAX DOOR OUTER HANDLE CAUTION MESSAGE ILLUMINATED DURING CLIMB THRU 26000 FT. RAN QRH AFTER PAX DOOR WARNING. COMPLIED WITH QRH. DECLARED AN EMERGENCY, DESCENDED TO 10000 FT, WARNING WENT AWAY & PRESSURIZATION NORMAL. R & R PAX DOOR HARNESS IAW AMM 52-70-04. COMPLIED WITH OPS TEST OF PAX DOOR. OPS CHECKED GOOD.

Part: PSEU — FAULTY (LANDING GEAR) · airframe 26,788 hrs · 26,617 cycles

4071 AFTER LOWERING LANDING GEAR RECEIVED WOW INPUT CAUTION MSG. FOLLOWED BY WOW OUTPUT CAUTION MSG. COMPLIED WITH QRH. LANDING, ROLLOUT & BRAKE TEMPS ARE NORMAL. NWS WN ARM. INTERROGATED PSEU & FOUND, NO COMM, FAULT MSG. R & R PSEU IAW AMM 32-61-01. OPERATIONS CHECKED GOOD. OPERATIONS CHECK OF NWS GOOD IAW 32-50-00.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 32,549 hrs · 31,622 cycles

PASSENGER DOOR INTERCOSTAL CRACKED BETWEEN FS 338.0 & FS 347.25 ADJACENT TO UPPER CATCH PIN. R & R DAMAGED INTERCOSTAL PN 601R1902-318S.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 32,549 hrs · 31,622 cycles

CARGO DOOR FWD STOP FITTING ATTACHMENT BRACKET & FLOOR BEAM FS 589 ARE CRACKED. REPAIRED CRACKED FLOOR BEAM FS 589 LBL IAW STS EA 15-2013-530. R & R UNSERVICEABLE FWD STOP FITTING ATTACH BRACKET WITH NEW SERVICEABLE BRACKET IAW CRJ 200 SRMS 51-24-21. 51-42-21, 51-62-15 & 53-61-23.

Part: SKIN — DAMAGED (LT WING) · airframe 32,549 hrs · 31,622 cycles

LEFT WING SKIN FWD OF FLIGHT SPOILER DAMAGED ALSO INBD & OTBD SUPPORT CHANNELS WERE DAMAGED. REPLACED SKIN & CHANNELS IAW CRJ 200 SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 32,549 hrs · 31,622 cycles

RIGHT INBD FLAP VANE LE CHAFED. R & R RT INBD FLAP VANE OTBD LE PN 601R14303-44.

Part: SKIN — CHAFED (PAX DOOR) · airframe 32,549 hrs · 31,622 cycles

PASSENGER DOOR INNER SKIN HAS DEEP CHAFE FROM SPRING STRUT ATTACH BRACKET HARDWARE BELOW LOWER FOLDING STEP. PERFORM CUT OUT & DOUBLER REPAIR IAW EA 15-2013-532.

Part: SEAL DEPRESSOR — GOUGED (FUSELAGE) · airframe 32,549 hrs · 31,622 cycles

TWO EACH GOUGES AT SEAL DEPRESSION AREA IN PROXIMITY OF BOTH LOWER SERVICE DOOR STOPS. R & R SERVICE DOOR SEAL DEPRESSION IAW 51-41-02.

Part: MOUNT — CRACKED (FUSELAGE) · airframe 32,549 hrs · 31,622 cycles

AIRCRAFT GND ADAPTER MOUNT IS CRACKED. R & R ACFT GND MOUNT ADAPTER PN 600-33283-33 IAW CRJ SRM 51-42-06.

Part: PLATE — UNSERVICEABLE (FUSELAGE) · corrosion level 2 · airframe 32,549 hrs · 31,622 cycles

FOUND AFT OTBD FOOT MOUNTING PLATE TO BE OUT OF SERVICEABLE LIMITS. REMOVED UNSERVICEABLE PLATE, FABRICATED & INSTALLED SERVICEABLE FOOT MOUNTING PLATE IAW CRJ 200 SRM 51-42-13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,549 hrs · 31,622 cycles

FLOOR SUPPORT BEAM HAS CORROSION AT RT OTBD END AT SERVICE DOOR SILL AFT EDGE FS 349. BLENDED CORROSION & FOUND TO BE WITHIN LIMITS IAW REO 601R-53-21-2496.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 32,549 hrs · 31,622 cycles

REPAIR 4A H STAB CLOSING RIB 601R-55-11-462. REPAIR IAW REO 601R-55-11-477 DATED 12-27-13.

Part: ANCHOR — CORRODED (PAX DOOR) · corrosion level 2 · airframe 32,549 hrs · 31,622 cycles

PASSENGER DOOR AFT ANCHOR HAS CORROSION AROUND SCREW HEADS. REMOVED & REPLACED PAX DOOR AFT ANCHOR FITTING COVER PLATE IAW CRJ 200 SRM 51-41-02.

Part: CLEAT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 32,549 hrs · 31,622 cycles

CARGO TIE DOWN CLEET CORROSION AT LBL 27 FS 559+112. R & R CARGO TIE DOWN CLEET AT LBL 27 FS 559+112 IAW CRJ 200 SRM 51-41-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,549 hrs · 31,622 cycles

AFT FS 621 BULKHEAD OBLIQUE ANGLE CRACKED AT STRINGER 14R. R & R IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 32,549 hrs · 31,622 cycles

AFT SIDE OF FS 621 PRESS BULKHEAD AT STRINGER HAS CRACKED INTERCOSTAL COMMON TO MOLD LINE SKIN. FOUND LENGTH OF CRACK 1.063 WITHIN ALLOWABLE LIMITS IAW CRJ 200 SB 601R-53-048.

Part: HINGE BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,549 hrs · 31,622 cycles

AFT LAVATORY SERVICE DOOR LOWER HINGE ARM BRACKET HAS CORROSION. FABRICATED NEW BRACKET & INSTALLED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,549 hrs · 31,622 cycles

FUSELAGE STATION 280 AT LBL 9 CLIP CRACKED. REMOVED CRACKED FS 280 CLIP LBL 9 & REPLACED WITH SERVICEABLE FS 280 LBL 9 CLIP.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 32,549 hrs · 31,622 cycles

AFT SIDE OF FS 621 PRESS BULKHEAD AT STRINGER 16L HAS CRACKED INTERCOSTAL COMMON TO MOLD LINE SKIN. FOUND LENGTH OF CRACK 1.406" WITHIN ALLOWABLE LIMITS IAW CRJ 200 SB 601R-53-048.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,549 hrs · 31,622 cycles

AFT SIDE OF FS 621 PRESS BULKHEAD AT STRINGER 14R CRACKED, COMMON TO SKIN. R & R IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,549 hrs · 31,622 cycles

FUSELAGE STATION 280 RBL 9 CLIP CRACKED. REMOVED UNSERVICEABLE FS 280 RBL 9 CLIP & REPLACED WITH SERVICEABLE FS 280 RBL 9 CLIP.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 32,549 hrs · 31,622 cycles

AFT SIDE OF FS 621 PRESS BULKHEAD AT STRINGER 13L HAS CRACKED INTERCOSTAL COMMON TO MOLD LINE SKIN. FOUND LENGTH OF CRACK 1.1875" WITHIN ALLOWABLE LIMITS IAW CRJ 200 SB 601R-53-048.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 32,549 hrs · 31,622 cycles

AFT SIDE OF FS 621 PRESS BULKHEAD AT STRINGER 15L HAS CRACKED INTERCOSTAL COMMON TO MOLD LINE SKIN. FOUND LENGTH OF CRACK .969 WITHIN ALLOWABLE LIMITS IAW CRJ 200 SB 601R-53-048.

Part: HOUSING — CRACKED (CARGO DOOR) · airframe 32,549 hrs · 31,622 cycles

CARGO DOOR HANDLE HOUSING CRACKED. R & R CARGO DOOR HANDLE.

Part: DRAG ANGLE — CRACKED (RT MLG) · airframe 32,549 hrs · 31,622 cycles

RIGHT DRAG ANGLE CRACKED FWD & AFT ENDS. R & R ANGLE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,549 hrs · 31,622 cycles

CORROSION FOUND ON PAX DOOR LOWER SILL. R & R PAX DOOR LOWER SILL.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 32,549 hrs · 31,622 cycles

LIGHTNING STRIKE DAMAGE ON LOWER FWD SKIN PANEL BTW BL 0.0 & RBL 3.8, FS 169. R & R LOWER FWD SKIN PANEL.

Part: ANGLE — CRACKED (E&E DOOR) · airframe 32,549 hrs · 31,622 cycles

AVIONICS BAY DOOR RT RAIL FWD MOUNT ANGLE IS CRACKED. R & R IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,549 hrs · 31,622 cycles

FLOOR BEAM AT FS 349 JUST INBD OF PAX DOOR HAS CORROSION. CORROSION REMOVED FROM STATION 349 FLOOR BEAM IAW CRJ200 SRM 51-21-06. REPLACED UNSERVICEABLE AFT SUPPORT BRACKET WITH SERVICEABLE SUPPORT BRACKET.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,549 hrs · 31,622 cycles

LEFT FLOOR SEAT TRACK SECTION FROM FS 409 TO FS 409+128 ON LBL 9 HAS CORROSION IN FIVE LOCATIONS. SEAT TRACK WAS FOUND TO BE OUT OF SERVICEABLE LIMITS. R & R SERVICEABLE FABRICATED SEAT TRACKS LBL 9 IAW CRJ 200 AMM 53-01-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 32,549 hrs · 31,622 cycles

FLOOR BEAM AT FS 349 JUST INBD OF PAX DOOR HAS CORROSION. CORROSION REMOVED FROM STATION 349 FLOOR BEAM IAW CRJ 200 SRM 51-21-06. REPLACED UNSERVICEABLE AFT SUPPORT BRACKET WITH SERVICEABLE SUPPORT BRACKET.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 32,549 hrs · 31,622 cycles

LEFT UNDERFLOOR STRUCTURE AT FS 484 HAS CRACK AT OTBD FLANGE UPPER END. REPAIR IAW REO 601R-53-41-059 REV B.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 32,549 hrs · 31,622 cycles

CARGO DOOR FWD TRACK SUPPORT ANGLE CRACKED AT CTR SUPPORT INTERCOSTAL. REMOVED OLD ANGLE, FABRICATED NEW SUPPORT ANGLE & INSTALLED.

Part: PLATE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 32,549 hrs · 31,622 cycles

SERVICE DOOR STEP PLATE HAS CORROSION ON UNDERSIDE OF PLATE. R & R SERVICE DOOR STEP PLATE.

Part: UNKNOWN — ODOR (CABIN) · airframe 29,837 hrs · 29,006 cycles

APU ON MEL, PERFORMED AN AIR START OF BOTH ENGINES. SHORTLY AFTER BRINGING PACKS ONLINE AND CLOSING PASSENGER DOOR COCKPIT AND CABIN FILLED WITH A HAZY SMOKE AND TOXIC ODOR. ODOR WAS NOT TYPICAL OF OIL IN PACKS. PASSENGER DOOR WAS OPENED AND PACKS TAKEN OFFLINE. A FEW MOMENTS LATER, BOTH ENGINES WERE SHUTDOWN. HAZE/ODOR DISSIPATED AND PASSENGERS REMAINED SEATED. SUSPECTED CAUSE WAS THE AIR CART, AS THIS ACFT WAS USED FOR PREVIOUS FLIGHT WITH NO ISSUES. PASSENGERS DEPLANED WHILE MX CAME OUT TO CHECK PACKS. EMPLOYED ALTERNATE AIR CART AND RAN PACKS. FAINT SMELL WAS DETECTED, BUT WAS TOLERABLE AND NO SMOKE WAS PRESENT. ELECTED TO BOARD AND RESUME FLIGHT. WHILE STILL ON GROUND THERE WAS NO SMOKE AND JUST A VERY LIGHT RESIDUAL ODOR. JUST PRIOR TO ACCELERATION SAME ODOR WAS DETECTED, BUT FAINTER THAN PREVIOUSLY EXPERIENCED ON GROUND. ONCE AGAIN IT DISSIPATED ENOUGH THAT CREW WAS COMFORTABLE CONTINUING THE FLIGHT. ON ARRIVAL, WHILE CONFIGURING AND BRINGING UP THRUST, THE SAME ODOR APPEARED. AFTER GATE ARRIVAL MX WAS CONTACTED AND INFORMED OF FLIGHT EVENTS. MX PERFORMED ENGINE RUNS WITH NO ODOR NOTED IAW AMM 71-00-00. ALL OPS CHECKS GOOD.

Part: UNKNOWN — SMOKE (CABIN & COCKPIT) · airframe 29,837 hrs · 29,006 cycles

PERFORMED AN AIR START OF BOTH ENGINES. AFTER BRINGING PACKS ONLINE AND CLOSING PAX DOOR COCKPIT AND CABIN FILLED WITH A HAZY SMOKE AND TOXIC SMELLING ODOR. PACKS TAKEN OFFLINE. BOTH ENGINES WERE SHUT DOWN. HAZE/ODOR DISSIPATED. MX CONTACTED. PAX DEPLANED WHILE MX CAME OUT TO CHECK PACKS. EMPLOYED ALTERNATE AIR CART AND RAN PACKS. FAINT SMELL WAS DETECTED, BUT WAS TOLERABLE AND NO SMOKE WAS PRESENT. ELECTED TO RESUME FLIGHT. JUST PRIOR TO ACCELERATION SAME ODOR WAS DETECTED, BUT FAINTER THAN PREVIOUSLY EXPERIENCED ON GROUND. ONCE AGAIN IT DISSIPATED ENOUGH THAT CREW WAS COMFORTABLE CONTINUING THE FLIGHT. ON ARRIVAL, WHILE CONFIGURING AND BRINGING UP THRUST, THE SAME ODOR APPEARED. MX PERFORMED ENGINE RUNS WITH NO ODOR NOTED PER AMM 71-00-00. ALL OPS CHECKS GOOD.

Part: INDICATOR — INACCURATE (ATTITUDE) · airframe 22,548 hrs · 22,475 cycles

AFTER DEPARTURE AT 80 KNOTS, NOTED STANDBY ATTITUDE INDICATING ZERO KNOTS. RETURNED TO DEPARTURE. PRUGED P3 SYS, REPLACED P3 DRAIN AND STANDBY IAS/ALT IAW AMM 34-12-01. OPS CHECKED GOOD. PITOT STATIC LEAK CHECK PASSED IAW AMM 34-11-00. OPS CHECK GOOD OK FOR SERVICE.

Part: INDICATOR — INOPERATIVE (AIRSPEED) · airframe 28,805 hrs · 27,956 cycles

AFTER DEPARTURE AT 80 KNOTS, NOTED STANDBY AIRSPEED INDICATING "0" KNOTS. RETURN TO DEPARTURE.

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 22,346 hrs · 22,272 cycles

ON APPROACH, RECEIVED SPOILERON & FLT SPOILERON CAUTION MESSAGE, FOLLOWED BY INBD & OTBD GROUND SPOILER MESSAGES. ALL HYD PRESSURES AT 3000 PSI AND QUANTITIES ARE NORMAL. C/W FIM RESET PROCEDURE = MESSAGE CLEARED.

Part: SEAT TRACK — CORRODED · airframe 27,644 hrs · 26,780 cycles

SEAT TRACK ON RBL 9 IN CARGO BAY FS 559+112 CORRODED. REMOVED UNSERVICEABLE SEAT TRACK AND REPLACED WITH NEW SERVICEABLE SEAT TRACK.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 21,576 hrs · 21,493 cycles

SPOILERON AND FLT SPOILERS AT CASS CAUTION MESSAGE DURING ARRIVAL FOLLOWED QRH CHECKLIST FOR BOTH LAND FLAPS 20. AFTER LANDING CAUTION MESSAGE WENT OUT AND RECEIVED INBD AND OTBD FAULT STATUS MESSAGE. PERFORMED FUNCTION CHECK OF SPOILER CONTROL SYS IAW 27-61-00-720. OPS CHECKED GOOD. NO FAULTS FOUND AT THIS TIME.

Part: FRAME — DENTED · airframe 27,644 hrs · 26,780 cycles

2ND FRAME INSIDE AEB COMPARTMENT- FWD FROM THE AEB DOOR CUT OUT IS DENTED AT ABOUT 5:00 POSITION. CUTOUT DAMAGED SECTION OF FRAME AND FABRICATED NEW PARTS IAW REO 601R-53-61-4333.

Part: CLEAT — CORRODED (BS 316.0) · corrosion level 2 · airframe 27,644 hrs · 26,780 cycles

PAX DOOR FWD AND AFT CLEATS ARE CORRODED, R & R.

Part: SEAT TRACK — CORRODED (FS 409) · corrosion level 2 · airframe 27,644 hrs · 26,780 cycles

RBL 9 2ND SECTION OF SEAT TRACK CORRODED. R & R SEAT TRACK.

Part: FLOORBEAM — CORRODED (FS 574 - 621) · airframe 27,644 hrs · 26,780 cycles

LBL 27.0 FLOORBEAM CAP BETWEEN FS 574.0 AND 621.0 HAS CORROSION AROUND NUTPLATE HOLES. REMOVED CORRODED LBL27 FLOORBEAM CAP BETWEEN FS 574.00 AND FS 621.00. THEN INSTALLED NEW SERVICEABLE FLOORBEAM IAW REO 601R-53-61-3778, REV A.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 27,644 hrs · 26,780 cycles

RT INBD FLAP VANE CHAFED 3 PLACES ON L/E. REPAIRED RT INBD FLAP VANE L/E AT 3 PLACES ( INBD, CTR, OTBD) IAW REO 601R-57-52-004, REV C, SRM 51-42-13, SRM 51-40-11.

Part: SKIN — CHAFED (RT AILERON) · airframe 27,644 hrs · 26,780 cycles

RT AILERON LWR L/E CHAFED IN 2 AREAS, R & R.

Part: SEAT TRACK — CORRODED (RBL9) · airframe 27,644 hrs · 27,680 cycles

4TH SECTION OF SEAT TRACK ON RBL 9 CORRODED IN NUMEROUS PLACES. REMOVED 4TH SECTIONOF SEAT TRACK ON RBL9 AND REPLACED WITH SERVICEABLE SEAT TRACK IAW AMM 53-01-11 & SRM 51-40-11, 51-21-11.

Part: SEAT TRACK — CORRODED (BS 615.0) · airframe 27,644 hrs

SEAT TRACK ON LBL9 AT FS 615.00 CORRODED. REMOVED SEAT TRACK ON LBL 9 AT FS 615.00. REPLACED WITH SERVICEABLE SEAT TRACK 601R38779-13 IAW AMM 53-01-11 & 51-40-11, 51-21-11.

Part: ATTACH FITTING — BROKEN (RT ELEVATOR) · airframe 27,644 hrs · 26,780 cycles

INBD ATTACH CLIP UNDER PANEL 344BB ON RT ELEVATOR BROKEN. R & R INBD ATTACH CLIP UNDER PANEL 344BB ON RT ELEVATOR IAW SRM 51-42-06.

Part: PANEL — DAMAGED (HORIZONTAL STAB) · airframe 27,644 hrs · 26,780 cycles

LEFT PCV PANEL HAS 2 HOLES THAT ARE ELONGATED (ON HORIZ STAB). REPAIRED BY FREEZER PLUG IAW REO 601R-55-11-400.

Part: CARGO TRACK — CORRODED (FS 559) · airframe 27,644 hrs · 26,780 cycles

SEAT TRACK IN CARGO BAY ON LBL 9 CORRODED AT FS 559+96 IAW AMM 53-01-11. R & R CARGO BAY SEAT TRACK AT FS 559+96 IAW AMM 53-01-11.

Part: STRUCTURE — CRACKED (POWER RECEPTICLE) · airframe 27,644 hrs · 26,780 cycles

AC GROUND EXTERNAL POWER CONNECTION SURROUND STRUCTURAL CRACKED ON AFT LOWER CORNER. R & R MOUNT BRACKET PN 600-33283-33 IAW SRM 51-42-13, 51-42-21, REO 601R-53-11-029, REV A.

Part: SKIN — GOUGED (RT ELEVATOR) · airframe 27,644 hrs · 26,780 cycles

RIGHT ELEVATOR UPPER L/E SKIN DAMAGED 3 SPOTS GOUGED ABD BENT. REPAIRED IAW REO 601R-55-21-112 AND REO 601R-55-21-345.

Part: SEAT TRACK — CORRODED (FS 559) · airframe 27,644 hrs · 26,780 cycles

SEAT TRACK IN CARGO BAY ON RBL 27 CORRODED AT FS 559+96. R & R SEAT TRACK IAW SRM 51-41-02 AND AMM 53-01-11.

Part: HINGE FITTING — GOUGED (HORIZONTAL STAB) · airframe 27,644 hrs · 26,780 cycles

RIGHT HORIZONTAL STAB NR 2 ELEVATOR HINGE FITTING GOUGED. REPAIRED RT HORIZONTAL STAB NR 2 ELEVATOR HINGE FITTING IAW REO 601R-55-11-399.

Part: SEAT TRACK — CORRODED (FS 606-615) · airframe 27,644 hrs · 26,780 cycles

SEAT TRACK IN CARGO BAY ON RBL 9 CORRODED AT FS 615. R & R SEAT TRACK AT FS 615, RBL9.

Part: SEAT TRACK — CORRODED (FS 544-559) · corrosion level 2 · airframe 27,644 hrs · 26,780 cycles

RIGHT SIDE WALL SEAT TRACK HAS CORROSION BETWEEN FS 544 TO 559. R & R SERVICEABLE SEAT TRACK ON RT SIDE WALL IAW AMM 53-01-11.

Part: MOUNT — CORRODED (FUSELAGE) · airframe 27,644 hrs · 26,780 cycles

WARDROBE ASSY APPEARS TO HAVE SLIGHT SURFACE CORROSION ON BOTTOM SIDE MOUNTS (3EA) R & R.

Part: SKIN — DENTED (FS 210-220) · airframe 27,644 hrs · 26,780 cycles

FUSELAGE SKIN DENTED. PERFORMED PERMANENT REPAIR TO RT SKIN BETWEEN FS 210-220, STR 11-12, BY FULLY INCORPORATING STS EA 10-2011-197, ISSUE DATE 12/13/11.

Part: SKIN — GOUGED (RT AILERON L/E) · airframe 27,644 hrs · 26,780 cycles

RIGHT AILERON UPPER L/E SKIN GOUGED AT INBD HINGE. FOUND DAMAGE TO BE PAINT ONLY. FOUND GOUGE ON INBD HINGE FITTING ON RT AILERON. REPAIRED RT AILERON INBD HINGE FITTING IAW REO 601R-57-61-395.

Part: HINGE FITTING — DAMAGED (RT AILERON) · airframe 27,644 hrs · 26,780 cycles

RT AILERON INBD HINGE FITTING ON WING DAMAGED. REPAIRED RT AILERON INBD HINGE FITTING ON WING IAW REO 601R-57-51-565.

Part: SEAT TRACK — CORRODED (FS 513.0) · airframe 27,644 hrs · 26,780 cycles

3RD SECTION OF SEAT TRACK ON RBL 9 CORRODED AT FS 513.00. R & R SECTION OF SEAT TRACK IAW AMM 53-01-11 & SRM 51-40-11.

Part: SEAT TRACK — CORRODED (FS 559) · airframe 27,644 hrs · 26,780 cycles

SEAT TRACK ON LBL 9 IN CARGO BAY AT FS 559+112 CORRODED. R & R SEAT TRACK AT LBL9 & FS 559 IAW AMM 53-01-11 & SRM 51-40-11.

Part: PANEL — CHAFED (LT WING) · airframe 27,644 hrs · 26,780 cycles

PANEL 599BB CHAFED, BLENDED OUT DAMAGE, FOUND DAMAGE TO BE WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.

Part: SKIN — CHAFED (RT AILERON L/E) · airframe 27,644 hrs · 26,780 cycles

RT AILERON UPPER L/E SKIN CHAFED BELOW PANELS 698JT, 698KT AND 698LT, BLENDED IAW REO 601R-57-60-013.

Part: ACTUATOR — CHAFED (LT WING TE FLAP) · airframe 27,644 hrs · 26,780 cycles

LEFT INBD FLAP CENTER VANE ACTUATOR CHAFED, BLENDED IAW REO 601R-57-52-1824.

Part: ACTUATOR — CHAFED (LT WING TE FLAP) · airframe 27,644 hrs · 26,780 cycles

LEFT INBD FLAP VANE OTBD ACTUATOR TUBE CHAFED, BLENDED IAW REO 601R-57-52-1824.

Part: HINGE FITTING — CHAFED (RT AILERON) · airframe 27,644 hrs · 26,780 cycles

CHAFING DAMAGE TO RT INBD HINGE BOX ATTACH LUG BLENDED DAMAGE IAW REO 601R-57-51-1562.

Part: SKIN — CHAFED (LT NACELLE) · airframe 27,644 hrs · 26,780 cycles

LEFT LOWER CORE COWL OUTER SKIN CHAFED BY FWD LATCHES LT LOWER CORE COWL OUTER SKIN. REPAIRED IAW CMM 71-12-01-300-822. REPAIRE NR SR104.

Part: HINGE FITTING — CRACKED (LT BUTTE DOOR) · airframe 27,644 hrs · 26,780 cycles

LEFT BUTTE DOOR 594ND AND 594JD HAS CRACKED HINGE PLATE AND END PLATE. REMOVED UNSERVICEABLE HINGE AND END PLATE AND INSTALLED SERVICEABLE HINGE AND END PLATE IAW SRM 51-42-06.

Part: SKIN — CHAFED (WING) · airframe 27,644 hrs · 26,780 cycles

LOWER WING SKIN BELOW PANEL 193AB LT & RT CORNER CHAFED. REPAIRED IAW REO 601R-57-21-880.

Part: FITTING — CRACKED (FS 484)

BATH TUB FITTING AT FS 484, RBL 9 CRACKED AT RADIUS, R & R IAW SRM.

Part: STRUCTURE — CHAFED (RT WING) · airframe 27,644 hrs · 26,780 cycles

RT APRON CHAFED FROM WING PANELS AT AFT WING STUB FAIRING, COMPLIED WITH REO 601R-53-41-341.

Part: SKIN — CHAFED (LT WING L/E) · airframe 27,644 hrs · 26,780 cycles

LEFT WING INBD L/E INNER SKIN AT INBD END CHAFED PG 79-3. REMOVED, FABRICATED, AND REINSTALL IAW FORM 412 SRM 51-42-06, 51-42-13, 51-22-00, 51-40-11, 51-42-15, 51-21-11, 51-25-06.

Part: STRUCTURE — CHAFED (RT WING) · airframe 27,644 hrs · 26,780 cycles

RIGHT AFT WING APRON CHAFED. REMOVED CHAFE IAW REO 601R-53-41-341.

Part: PANEL — CHAFED (WING) · airframe 27,644 hrs · 26,780 cycles

WING PANEL 699B CHAFED. REMOVED CHAFE IAW REO 601R-57-60-020.

Part: PANEL — CHAFED (WING) · airframe 27,644 hrs · 26,780 cycles

PANEL 699CB CHAFED. REMOVED CHAFE IAW REO 601R-57-60-020.

Part: SILL — CORRODED (BS 409-559) · airframe 27,644 hrs · 26,780 cycles

RIGHT FLOOR SILL CORRODED FROM 409+128 TO 559.00. REMOVED CORROSION IAW REO 601R-53-41-666.

Part: SILL — CORRODED (BS 409-559) · airframe 27,644 hrs · 26,780 cycles

FLOOR SILL BETWEEN 409.00+128 HAS CORROSION LT SIDE. REMOVED CORROSION IAW REO 601R-53-41-666.

Part: INTERCOSTAL — CRACKED (FS 484) · airframe 27,644 hrs · 26,780 cycles

CRACK CLIP ON INTERCOSTAL OTBD AT FS 484.0 OF RBL 27, R & R.

Part: INTERCOSTAL — CRACKED (FS 484) · airframe 27,644 hrs · 26,780 cycles

CRACK CLIP ON INTERCOSTAL INBD AT FS 484 OF RBL 36, R & R.

Part: BULKHEAD — CHAFED (FS 280) · airframe 27,644 hrs · 26,780 cycles

FS 280 AFT BULKHEAD RT SIDE CHAFED IN 2 PLACES FROM GALLEY COMPARTMENT DOOR. REPAIRED DAMAGE AT FS 280, AFT BULKHEAD RT SIDE IAW REO 601R-53-11-1727, REV E.

Part: HANDLE — CHAFED (CARGO DOOR) · airframe 27,644 hrs · 26,780 cycles

CARGO DOOR HANDLE CUT OUT CHAFED BLEND.

Part: LEVER — CHAFED (PAX DOOR) · airframe 27,644 hrs · 26,780 cycles

PAX DOOR FWD PULL IN LEVER CHAFED, BLENDED IAW REO 601R-52-11-524.

Part: BEAM — CHAFED (LT WING) · airframe 27,644 hrs · 26,780 cycles

LEFT FLAP INBD VANE ACTUATOR INBD BEAM CHAFED BLENDED IAW REO 601R-57-52-1824.

Part: FAIRING — LOOSE (LT JET PIPE) · airframe 27,644 hrs · 26,780 cycles

LEFT JET PIPE FAIRING ALL 2 NUT PLATE ASSY LOOSE. R & R WITH NEW FABBED 3 EA NUTPLATE ASSY`S ON LT JET PIPE FAIRING IAW CMM 20-42-06.

Part: SHROUD — CRACKED (RT WING OTBD L/E) · airframe 27,644 hrs · 26,780 cycles

RT WING OTBD L/E SHROUD CRACKED. FABRICATED REPLACEMENT SHROUD IAW SRM 51-24-26 & 51-40-11.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 20,554 hrs · 19,663 cycles

FLT 3607, FLAP FAIL MESSAGE GOING FROM FLAPS 20 T0 30. COMPLIED WITH QRH, LANDED UNEVENTFULLY WITH FLAPS AT 20 DEGREES. OPEN.

Part: LINKAGE — FOD (PAX DOOR) · airframe 17,000 hrs · 15,944 cycles

PAX DOOR WILL NOT OPEN FROM INSIDE OR OUT. (F/A AND THE CAPTAIN COULD NOT OPEN THE DOOR FROM THE INSIDE AND THE RAMP PERSON COULD NOT FRO THE OUTSIDE) INSPECTED DOOR LINKAGE, REMOVED FOD FOUND NO DEFECTS WITH LINKAGE. OPS CKS OK AT THIS TIME.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 23,924 hrs · 22,882 cycles

REQUEST INSPECTION OF ODOR IN COCKPIT AND GALLEY. C/A IN PROGRESS.

Part: ANGLE — CRACKED (BS 625) · airframe 16,805 hrs · 15,739 cycles

LT 625, OBLIQUE ANGLE CRACKED. R & R WITH SERVICEABLE OBLIQUE ANGLE PN 601-35012-51 AT LT FS625. ALL WORK DONE IAW SRM 51-40-11, 51-21-11, 51-25-06, 51-25-16, 51-42-21,51-22-00.

Part: RIB — CRACKED (RT WING) · airframe 23,128 hrs · 22,077 cycles

RT MLG WHEEL WELL BATT RIB CRACKED. REPAIRED RT MLG WHEEL WELL BATT RIB IAW REO 601R-57-51-046.

Part: STRINGER — DAMAGED (BS 324) · airframe 23,128 hrs · 22,077 cycles

LIGHTNING STRIKE DAMAGE AT STR 26L, FS 324 IS OUT OF ALLOWABLE LIMITS. REPAIRED LIGHTNING STRIKE DAMAGE AT FS 324.0, STR 26L IAW SRM 53-00-31.

Part: RIB — CRACKED (LT WING) · airframe 23,128 hrs · 22,077 cycles

LT MLG WHEEL WELL BATT RIB CRACKED. REPAIRED LT MLG WHEEL WELL BATT RIB IAW REO 601R-57-51-046.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 23,128 hrs · 22,077 cycles

PAX DOOR FRAME CRACKED BY ROLL MECHANISM AFT OF FWD DOOR EDGE. COMPLIED WITH REO 601R-52-11-1742.

Part: STIFFENER — CRACKED (BS 559) · airframe 23,128 hrs · 22,077 cycles

CRACK WAS FOUND ON VERT STIFFENER. LBL 9, FS 559 PERFORMED REO 601R-53-41-260. REPAIR IAW CUSTOMER REQUEST ON LT AND RT SIDES.

Part: DOOR FRAME — CRACKED (MAIN PAX) · airframe 23,128 hrs · 22,077 cycles

PAX DOOR FRAME CRACKED BY ROLL-LATCH MECHANISM FWD OF AFT DOOR EDGE. COMPLIED WITH REO 601R-52-11-402.

Part: ATTACH FITTING — OUT OF POSITION (BS 513) · airframe 23,128 hrs · 22,077 cycles

LT OVERWING AFT ATTACH LINK (DOGBONE FS 513) IS TOUCHING WING ATTACH FITTING ON INBD FWD SIDE COMPLIED WITH REO 601R-53-41-1132. FLY ON FOR 5000 FLT HOURS WITH 1000 HR RE-INSPECT INTERVALS.

Part: FRAME — CORRODED (BS 319.7) · airframe 23,128 hrs · 22,077 cycles

CORROSION ON FRAME 319.70 AT BL 0. REMOVED AND REPLACED LOWER FRAME SECTOR.

Part: PANEL — DAMAGED (FUSELAGE) · airframe 23,128 hrs · 22,077 cycles

OVERWING RT PANEL 162FL HAS COM DAMAGE LOWER LT CORNER. REPAIRED THE LT LOWER CORNER ON THE OVERWING RT PANEL 162FL IAW REO 601R-57-82-354.

Part: SILL — CORRODED (BS 319.7) · corrosion level 2 · airframe 23,128 hrs · 22,077 cycles

SERVICE DOOR LOWER SILL UNDERNEATH STEP PLATE HAS SIGNS OF CORROSION. REMOVED SERVICE DOOR LOWER SILL FABRICATED REPLACEMENT IAW SRM 51-42-34, 51-42-13, 51-42-21 AND 51-42-06.

Part: PANEL — CRACKED (VERTICAL STAB) · airframe 23,128 hrs · 22,077 cycles

FWD CORNER OF PANEL 326BL CRACKED OFF. (VISOR PANEL FAIRING). TRIMMED DAMAGE IAW REO 601R-55-32-246.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 23,128 hrs · 22,077 cycles

PAX DOOR LOWER AFT EDGE MEMBER IS CRACKED. REPAIRED DAMAGE ON PAX DOOR LOWER AFT EDGE MEMBER IAW REO 601-51-11-279.

Part: SEAT TRACK — WORN (BS 250) · airframe 23,128 hrs · 22,077 cycles

CO-PILOTS INBD AND OTBD SEAT RAILS ARE WORN. REMOVED AND REPLACED CO-PILOTS INBD AND OTBD SEAT TRACKS IAW SRM 51-42-21.

Part: SEAT TRACK — WORN (BS 237.67) · airframe 23,128 hrs · 22,077 cycles

PILOTS INBD AND OTBD SEAT RAILS WORN. REMOVED AND REPLACED PILOTS INBD AND OTBD SEAT RAILS IAW SRM 51-42-21.

Part: STIFFENER — CRACKED (APU ENCLOSURE) · airframe 23,128 hrs · 22,077 cycles

APU ENCLOSURE DOOR EXTERNAL STIFFENERS CRACKED AT UPPER WELD. REPAIRED CRACKS (2 EA) IAW REO 601R-49-11-070.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,128 hrs · 22,077 cycles

FS 280, FLOOR SUPPORT UPPER CAP CRACKED AT RBL 10.0 AND LBL 10.0. REPAIRED IAW REO 601R-53-11-136.

Part: SUPPORT ANGLE — CRACKED (BS 280) · airframe 23,128 hrs · 22,077 cycles

FS 280 FWD SUPPORT ANGLE BENEATH COCKPIT FLOORBOARD 221ALF CRACKED. REMOVED DAMAGE ANGLE, DUPLICATED SERVICEABLE ANGLE AND INSTALLED SERVICEABLE ANGLE.

Part: ATTACH ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 23,128 hrs · 22,077 cycles

ATTACH ANGLE AT FS 320.10 IN LWR PAX DOOR CORRODED RII REQUIRED. REMOVED CORRODED ATTACH ANGLES, DUPLICATED PARTS AND INSTALLED NEW SERVICEABLE PARTS.

Part: ATTACH ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 23,128 hrs · 22,077 cycles

ATTACH ANGLES AT FS 338.00 IN LWR PAX DOOR CORRODED. REMOVED CORRODED ATTACH ANGLE, DUPLICATED PART AND INSTALLED NEW SERVICEABLE ANGLE.

Part: BRACKET — CRACKED (BS 718) · airframe 23,128 hrs · 22,077 cycles

HYD SYS NR 1 PRESSURE/RETURN FILTER MANIFOLD MOUNT BRACKET CRACKED IN LOWER AFT RADIUS. REPAIRED HYD SYS NR 1 PRESSURE/RETURN MANIFOLD MOUNT BRACKET IAW REO 601R-53-62-031. (K)

Part: ANGLE — CRACKED (LT WING) · airframe 23,128 hrs · 22,077 cycles

LT WING OTBD ATTACH ANGLE UNDER ACCESS PANEL 520ML IS CRACKED. REMOVED CRACKED ATTACH ANGLE FROM LT WING OTBD UNDER ACCESS PANEL 520ML AND INSTALLED SERVICEABLE BRACKET PN 600-12045-11 IAW SRM 51-41-061.

Part: ANGLE — CRACKED (LT WING) · airframe 23,128 hrs · 22,077 cycles

LT WING OTBD ATTACH ANGLE UNDER ACCESS PANEL 520 ML CRACKED. REMOVED CRACKED ATTACH ANGLE FROM LT WING, OTBD UNDER ACCESS PANEL 520 ML AND INSTALLED SERVICEABLE BRACKET PN 600-12045-11, IAW SRM 51-41-061. (K)

Part: PANEL — CRACKED (LT WING) · airframe 23,128 hrs · 22,077 cycles

LT OTBD L/E INNER SKIN PANEL CRACKED. REPLACED LT OTBD L/E INNER SKIN PANEL IAW SRM 51-42-06 AND SRM 51-42-13. (K)

Part: STIFFENER — CRACKED (RT ENGINE) · airframe 23,128 hrs · 22,077 cycles

RT JETPIPE 2ND RIB CRACKED. REAPRED RT JETPIPE 2ND RIB IAW CMM TASK 78-11-00-300-810-A01. REPAIR SRS 042.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 22,823 hrs · 21,786 cycles

PASSENGER DOOR DIFFICULT TO OPEN FROM OUTSIDE. INSPECTED AND LUBED PASSENGER DOOR LATCHING MECHANISM. OPS CK GOOD IAW AMM 52-11-00-05. (K)

Part: DOOR — STUCK (MAIN PAX) · airframe 22,639 hrs · 21,597 cycles

PAX DOOR WILL NOT OPEN FROM OUTSIDE. HART TO OPEN FROM INSIDE PLACARDED AND PLACED ON MEL. INSTALLED NEW HANDLE LATCH ASSY IAW AMM 52-11-21 HANDLE NOW WORKS BUT DOOR IS STILL HARD TO OPEN. FURTHER T/S REQUIRED. STOWED AND OPERATED INNER AND OUTER HANDLE ON PAX DOOR IAW AMM 52-10. DOOR OPS CHECKS NORMALLY. LUBED OUTER HANDLE IAW AMM 52-11. OK FOR SERVICE. (K)

Part: SEAL — MISSING (SERVICE DOOR) · airframe 22,320 hrs · 21,300 cycles

LOUD SQUEAL COMING FROM SERVICE DOOR WHEN PSI`D AT ALTITUDE. FOUND 2 AREAS ON SERVICE DOOR SEAL STRIKER MISSING SEALANT. REAPPLIED MISSING SEALANT IAW AMM 51 STANDARD PRACTICES. (K)

Part: COMPUTER — MALFUNCTIONED (FUEL SYSTEM) · airframe 21,519 hrs · 20,510 cycles

REFUEL SPR WILL NOT FUEL WING TANKS IN AUTO OR MANUAL. REMOVED AND REPLACED FUEL SYS COMPUTER, OPS CHECK GOOD. REMOVED AND REPLACED REFUEL/DEFUEL PANEL. OPS CHECK GOOD. REMOVED AND REPLACED REFUEL/DEFUEL PANEL HARNESS. OPS CHECK GOOD. 3 TANKS CONFIG COMPUTER, PN 736-643-10, SN 0933, TSO=12283, CSO=12230, PANEL PN 798-144-5, SN 0684, TSO=11159, CSO=10415.

Part: RETAINING CLIP — OUT OF POSITION (APU) · airframe 20,830 hrs · 19,855 cycles

WHILE SERVICING APU SMELL NOTICED OPENED PANEL RAN APU. FOUND APU INLET BELLOWS RETAINING CLIP RT SIDE SLID AFT AND CHAFED HOLE IN METERED FUEL LINE TO NOZZLES. DRIPS ON IGNITER BOX. R&R FUEL LINE, REPOSITIONED RETAINING CLIP AND PLACED SPIRAL WRAP ON FUEL LINE BEHIND CLIP.

Part: DOOR — STUCK · airframe 20,076 hrs · 19,133 cycles

CREW REPORTS PASSENGER DOOR UNABLE TO OPEN FROM OUTSIDE. INSPECTED PASSENGER DOOR LATCH MECHANISM, INNER AND OUTER HANDLES PER AMM 52-11-02, 52-11-03. REMOVED PUSH-PULL RODS AND CLEANED AND LUBED ROD ENDS. REMOVED, CLEANED AND LUBED INNER AND OUTER HANDLES REF 12-20-52. NO DEFECTS FOUND, DOOR OPERATES SMOOTHLY. PASSENGER DOOR OPS CHECK GOOD. REF 52-11-23.

Part: CONTROL COLUMN — LOOSE (COCKPIT) · airframe 19,374 hrs · 18,466 cycles

REQUEST INSPECTION OF FIRST OFFICER`S CONTROL COLUMN FOR SUSPECTED EXCESSIVE PLAY IN NEUTRAL POSITION. PERFORMED OPS CHECK OF ELEVATOR CONTROL SYSTEM USING PITCH FEEL CHECK IAW AWAC SUPPLEMENT 2006-004A. OPS CHCEK GOOD. NO DEFECTS NOTED. (A)

Part: O-RING — LEAKING (APU FUEL LINE) · airframe 19,202 hrs · 18,301 cycles

STRONG FUEL ODOR THROUGHOUT CABIN AND COCKPIT SOMETIME AFTER APU STARTED ON ARRIVAL. FOUND APU FUEL LINE LEAKING. WITH APU OFF, FUEL LEAK STOPS. REF 201527/4 FOR MEL. R&R LOWER SOV ELBOW & O-RING IAW AMM 49-31-01. OPS AND LEAK CHECK GOOD.

Part: HANDLE — DAMAGED (PARKING BRAKE)

PARKING BRAKE HANDLE OCCASIONALLY SLIPS OUT OF POSITION. (M)

Part: HINGE — CRACKED (PAX DOOR) · airframe 18,279 hrs · 17,417 cycles

PAX DOOR UPPER FOLDING STEP, LOWER HINGE IS CRACKED. PAX DOOR UPPER FOLDING STEP, LOWER HINGE REPLACED IAW SRM 51-41-00. (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,279 hrs · 17,417 cycles

LT AND RT ANGLES CRACKED ON REAR PRESSURE BULKHEAD AFT SURFACE. (M) LT AND RT ANGLES ON AFT PRESSURE BULKHEAD (AFT FACE) AT FS 622, WL 73 TO 75, BTW STR 16 AND 17 INSTALLED AS IAW SRM 51-42-20. (K)

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 18,279 hrs · 17,417 cycles

FLOORBEAM AT FS 280 IS CRACKED AT LBL 9 AND RBL 9 CRACK AT LBL 9 IS .400 INCH CRACK AT RBL 9 IS 1.200 INCH. (M) FLOORBEAM REPAIRED IAW REO 601R-53-11-171 REV D. (K)

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 18,279 hrs · 17,417 cycles

CRACK FOUND ON FLOOR STRUCTURE FS 621, LBL 45 CRACK LENGTH IS .500 INCH. FLOOR SUPPORT AT FS 621.00 LBL 45 REPAIRED IAW REO 601R-53-61-117, REV C. (K)

Part: BRACKET — CRACKED (FUSELAGE) · airframe 18,274 hrs · 17,417 cycles

CRACK FOUND ON 4 BRACKET FS 280 LBL 9 AND RBL 9 CRACK LENGTH IS 1 INCH. (M) 3 BRACKETS REPLACED ON FS 280, LBL 9, OB AND IB AND RBL 9 OB IAW REO 601R-53-11-171 REV-D. BRACKET REPLACED ON FS 280, RBL 9, IB IAW CRJ 200, SRM 51-42-06. (K)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 18,279 hrs · 17,417 cycles

PAX DOOR STAIR ASSY, AFT DRAG ANGLE IS CRACKED. REPAIRED IAW CRJ200, REO 601R-52-11-513 REV (A). (K)

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · corrosion level 2 · airframe 18,279 hrs · 17,417 cycles

CORROSION FOUND ON FLOOR SUPPORT FS 589 TO 621, LBL 27. JOB PERFORMED ON FLOOR SUPPORT FS 589 TO 621, LBL 27 IAW REO 601R-53-61-2439. (K)

Part: SUPPORT CHANNEL — CRACKED (CARGO DOOR) · airframe 18,279 hrs · 17,414 cycles

FOUND CARGO DOOR FORWARD TRACK LOWER SUPPORT CHANNEL P/N 601R35050-25 FOUND CRACK APPROX .500 LONG 1 EACH. (M) CARGO DOOR FWD TRACK, LOWER SUPPORT CHANNEL. FABRICATED IAW SRM 51-24-16, CRACKED SUPPORT CHANNEL REMOVED IAW SRM 51-42-06, FABRICATED SUPPORT CHANNEL INSTALLED IAW SRM 51-42-06. (K)

Part: BULKHEAD — CRACKED (BS 202) · airframe 18,279 hrs · 17,417 cycles

CRACK FOUND ON T FWD PRESSURE BULKHEAD PARKING BRAKE CABLE HOLE APPROX .650 INCH LONG. FWD PRESSURE BULKHEAD AT FS 202.00, LBL 23.71. REPAIRED IAW REO 601R-53-11-563. (K)

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 18,279 hrs · 17,417 cycles

ON PAX DOOR, CRACK FOUND ON PASSENGER EDGE MEMBER. (M) PAX DOOR ON PASSENGER EDGE MEMBER REPAIRED IAW REO 601R-52-11-279. (K)

Part: DCU — MALFUNCTIONED (NR 2) · airframe 18,190 hrs · 17,330 cycles

RIGHT ENGINE N2 FLUCTUATION INFLIGHT. COMPLIED WITH QRH. N2 SPIKE OVER 104 PERCENT AT LEAST TWO TIMES WITH POWER REDUCED. OAT -6. NO VIBE GAUGE INDICATION. DIVERTED TO ORF. FOUND DCU NR 2 CAUSING N2 FLUCTUATING INDICATION. REMOVED AND REPLACED DCU NR 2 IAW AMM 31-41-04. OPS CHECK GOOD. (M)

Part: DOOR — LACK OF LUBE (MAIN PAX)

UNABLE TO OPEN MAIN PASSENGER DOOR. AFTER MULTIPLE ATTEMPTS, DOOR OPENED. OPERATED DOOR SEVERAL TIMES. DOOR APPEARS TO OPERATE NORMALLY. PLACED ON MEL. REF LOG 177995/2 CLEANED AND LUBED PASSENGER DOOR. PERFORMED OPS CHECK OF PASSENGER DOOR SEVERAL TIMES. OPS CHECK GOOD IAW 52-11-00. (M)

Part: UNKNOWN — ODOR (LAVATORY) · airframe 17,177 hrs · 16,364 cycles

LAV SMOKE TOILET MESSAGE APPEARED ON FINAL APPROACH. F/A REPORTED SMOKE AND STRONG ELECTRICAL ODOR COMING FROM CENTER OVERHEAD. APU AND PACKS ON. SMOKE DISSIPATED 3-5 MINUTES AFTER INDICATION. REMOVED CEILING PANELS. INSPECTED LIGHT FIXTURES AND WIRING. FOUND NO EVIDENCE OF BURNING OR ARCING IAW AMM 20-10-00. RAN AC PACKS FOR (2) HOURS. NO ODOR/ SMOKE NOTED. (K)

Part: APU — SMOKE (AFT) · airframe 17,177 hrs · 16,364 cycles

AFTER TRANSFERRING BLEEDS TO APU, THERE WAS A FAINT ODOR IN THE COCKPIT, ENGINES AT IDLE, (SMOKE TOILET) MESSAGE ON ED 1. MESSAGE CLEARED ON RUNWAY. FA REPORTS SMOKE AT CEILING AT ROW 11 AND 12. REPORTS SMOKE AT CEILING AT ROW 11 AND 12 REMOVED AND REPLACED APU ASSEMBLY IAW 49-10-00. OPS LEAK CHECK GOOD. (K)

Part: WIRE — SHORTED (GLARESHIELD)

CPLT ROLL COMMAND MESSAGE ON ED2 IN FLIGHT. GREEN CPLT ROLL LIGHT ILLUMINATED ON GLARESHIELD. COMPLIED WITH QRH. ROLL DISCONNECT HANDLE PULLED. EMERGENCY LANDING DECLARED. (M) [07-20-07] ISOLATED SHORT TO IB L/E (LT) REPAIRED WIRE CN619A22 AND CN620AZZ IAW WM 20-11-60, OPS CHECK GOOD. REF 16650-3 FOR L/E SEALANT. (K)

Part: ANGLE — CRACKED (RUDDER)

RUDDER SYSTEM (MID SPAR) ANGLE P/N 600-92638-1 AT LEFT AFT SIDE OF VS 67.5 PERCENT FRAME CRACKED APPROX .5 INCH LENGTH AT TOP INBOARD ATTACH RIVET. MAINTENANCE FABRICATED NEW ANGLE FROM 7075T6511 PO NR 74697/1 PER DRAWING 600-92638 AND INSTALLED IAW CRJ SRM 51-25-00, 51-42-06, 51-42-21 AND 51-41-02. (M)

Part: ATTACH ANGLE — CRACKED (RT WING)

ATTACHMENT ANGLE P/N 600-12025-8 FOR RIGHT WING L/E PANEL 620JT CRACKED AT UPPER AND LOWER CORNER WS 139.54 CRACKS APPROX .2 INCHES LONG. MAINTENANCE REPLACED ATTACHMENT ANGLE WITH NEW.

Part: ATTACH ANGLE — CRACKED (LT WING)

ATTACHMENT ANGLE P/N 600-12045-12 FOR WING L/E PANEL 630JT CRACKED AT UPPER AND LOWER CORNERS WS 149.58 CRACKS APPROX .2 INCH LONG. MAINTENANCE REPLACED ATTACHMENT ANGLE WITH NEW P/N 600-12045-12 IAW CRJ200 AMM 20-21-00-910-801. (M)

Part: DOOR — LACK OF LUBE (MAIN PAX)

PASSENGER DOOR WILL NOT OPEN FROM OUTSIDE. PLACARDED AND PLACED ON MEL. INSPECTED AND FOUND SEVERAL PUSH RODS SEIZED UP. APPLIED LUBRICANT TO AFFECTED AREAS IAW CRJ 12-20-52, OPS CHECK GOOD AT THIS TIME. REMOVED FROM MEL. (M)

Part: PDU — CONTAMINATED (THRUST REVERSER)

LEFT THRUST REVERSER UNSAFE CAUTION MESSAGE AND POSSIBLE DEPLOYMENT AT ROTATION. AIRCRAFT SHUDDERED. MESSAGE CLEARED AT 1000 FEET, NORMAL FLIGHT THEREAFTER. REMOVED AND REPLACED NR 1 ENGINE THRUST REVERSER POWER DRIVE PDU 9PDU FULL OF WATER, DRAINED UPON ARRIVAL. (M)

Part: A/C PACK — ODOR (LEFT)

WHEN AIRBORNE NOTICED EXHAUST ODOR FROM GASPERS IN FLIGHT DECK, LEFT PACK UNRESPONSIVE TO MANUAL OR AUTO MODE. TEMP 23 DEGREES CELSIUS, REDUCED AIRFLOW IN FLIGHT DECK WITH LT PACK ON. SHUTDOWN LT PACK PROCEEDED WITH SINGLE PACK. NO MESSAGE NOTED. ODOR CLEARED. PLACED ON MEL, NO EXHAUST ODOR WITH PACK OFF. (M)

Part: ACTUATOR — MALFUNCTIONED (RT FLAP)

FLAPS FAIL CAS MESSAGE IN FLIGHT. FLAPS STUCK AT ZERO LANDING WEIGHT 42,000 LBS. BTMS MAX READING 2, ALL IN GREEN. PLACED ON 72 HOUR FLAP WATCH, FECU NEEDS INTERROGATION. REPLACED RIGHT FLAP ACTUATORS AND FLEX DRIVE SHAFTS. (M)

Part: DRIVE SHAFT — FAILED (FLAP DRIVE SYS) · airframe 13,824 hrs · 13,158 cycles

IB TO MSP FLAP FAIL MESSAGE ILLUMINATED WHEN FLAP SELECTED TO 8 DEGREES. ACCOMPLISHED ZERO FLAP LANDING IAW CHECKLIST. HIGHEST TEMP= 5- ALL GREEN. REMOVED AND REPLACED LT FLEX SHAFT 1 THRU 4 IAW AMM. OPS CHECK GOOD AT THIS TIME. (K)

Part: SKIN — CORRODED (LT WING) · airframe 13,501 hrs · 12,865 cycles

LT WING LOWER PLANK ACCESS HOLE NR2 UNDER PNL 510AB AT WS 12.245 HAS CORROSION ON IB SIDE APPROX 3 INCH L X .1 INCH W X .004 DEEP IN NON CRITICAL AREA. MAINTENANCE REPAIRED WING PLANK ACCESS HOLE AT WS 12.245 IAW REO. (K)

Part: SKIN — DAMAGED (BS 640-700) · airframe 13,501 hrs · 12,865 cycles

DAMAGE TO FUSELAGE SKIN AT FS640-FS700 STRINGER 18, 19 LT SIDE. MAINTENANCE REMOVED DAMAGE SKIN BETWEEN FS 640- FS 700 AND STRINGER 18 - 19L. FABRICATED DOUBLER AND FILLERS AND INSTALLED IAW EO. (K)

Part: SELECTOR VALVE — MALFUNCTIONED (NLG)

GEAR DISAGREE WARNING IN FLIGHT COMPLIED WITH QRH, LANDED NORMAL. REMOVED AND REPLACED GEAR SELECTOR VALVE IAW AMM 32-33-10. PERFORMED GEAR EXTENSION AND RETRACTION TEST IAW AMM 32-30-00. LEAK AND OPS CHECK GOOD. (M)

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE)

AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO ORD. PER MEL 21-24-06-02 SECURED OVERBOARD VALVE IN THE CLOSED POSITION. PERFORMED OPS TEST, NO DISCREPANCIES NOTED. (M)

Part: THRUST REVERSER — OBSTRUCTED (RT ENGINE)

AFTER APPLICATION OF TAKEOFF POWER RT REVERSER UNLOCK CAS MESSAGE. ABORTED TAKEOFF PRIOR TO 80 KNOTS. ALL BRAKE TEMPS NORMAL. FOUND ICE ON THRUST REVERSER NOT ALLOWING THRUST REVERSER TO STOW AND LOCK. ON-CALL DEACTIVATED THRUST REVERSER AIRCRAFT FERRIED TO ORD AND PLACED ON MEL. REACTIVATED THRUST REVERSER SYSTEM, OPS CHECK NORMAL. CLEARED MEL. (M)

Part: THRUST REVERSER — FROZEN (RIGHT) · airframe 11,193 hrs · 10,792 cycles

AFTER APPLICATION OF TAKEOFF POWER RT REVERSER UNLOCK CAS MESSAGE. ABORTED TAKEOFF PRIOR TO 80 KNOTS. ALL BRAKE TEMPS NORMAL. FOUND ICE ON THRUST REVERSER NOT ALLOWING THRUST REVERSER TO STOW AND LOCK. ON-CALL DEACTIVATED THRUST REVERSER, AIRCRAFT FERRIED AND PLACED ON MEL.

Part: WINDSHIELD — FAILED (COCKPIT)

LEFT WINDSHIELD SHATTERED FL20,000 DESCENT LEFT FORWARD PRESSURIZATION NORMAL. REPLACED LEFT WINDSHIELD PER AMM 56-11-01, LEAK AND OPS CHECK GOOD. (M)

Part: STRUCTURE — CHAFED (BULKHEAD)

FOUND Z MEMBER CHAFED IN AFT EQUIPMENT BAY AT FS 625, BL0, WL 136, ON AFT SIDE OF AFT PRESSURE BULKHEAD. BLENDED CHAFED AREA. PERFORMED NDT INSPECTION. FABRICATED AND INSTALLED A REPAIR ANGLE IAW BRAS EO 601R-53-4884A. (M)

Part: CHANNEL — CHAFED (FUSELAGE)

MWC 69 - Z-MEMBER IS CHAFED IN AFT EQUIPMENT BAY AT FS 625, BL0, WL 136, ON AFT SIDE OF AFT PRESSURE BULKHEAD. BLENDED CHAFED AREA. PERFORMED NDT INSPECTION. FABRICATED AND INSTALLED A REPAIR ANGLE IAW BRAS EO 601R-53-4884A. (M)

Part: FRAME — CRACKED (FUSELAGE)

RIGHT FS 718 BETWEEN STRINGERS 11 AND 12 HAS CRACK ON FRAME FLANGE, WORK ORDER 63453 MAINTENANCE WORKCARD 24. TRIMMED OUT SECTION OF FRAME FLANGE, PERFORMED LPI OF CUT LINES. FABRICATED FILLER FROM 2024-T3 .040 INCH, WVAC PO NR 33626/1. FABRICATED REPAIR ANGLE FROM P/N 600-36030-24 AND INSTALLED REPAIR PARTS IAW 601R-61-143 REV A. (M)

Part: FRAME — CRACKED (FUSELAGE)

FOUND RIGHT FS 718 BETWEEN STRINGERS 11 AND 12 HAS A CRACK ON FRAME FLANGE. TRIMMED OUT SECITON OF FRAME FLANGE, PERFORMED LPI OF CUT LINES TO VERIFY ALL DAMAGE WAS REMOVED AND NO CRACKS EXIST. FABRICATED FILLER AND REPAIR ANGLE AND INSTALLED REPAIR PARTS IAW BOMBARDIER 601R-53-61-193. REV A. (M)

Part: TRIM SWITCH — FAILED (RUDDER)

RUDDER TRIM FAILED, NOSE LEFT. REMOVED AND REPLACED RUDDER TRIM SWITCH. (M)

Part: SWITCH — FAILED (COCKPIT)

RUDDER TRIM FAILED, NOSE LEFT. REMOVED AND REPLACED RUDDER TRIM SWITCH. (M)

Part: BOLTS — LOOSE (ELEVATOR CONTL)

DURING COMPLIANCE WITH MESA FCD 95-32, TWO BOLTS ON THE PILOTS SIDE ELEVATOR OUTPUT LEVER AND FIVE BOLTS ON THE CO-PILOTS SIDE ELEVATOR OUTPUT LEVER, P/N 82710093103, WERE FOUND TO BE LOOSE. NO APPARENT DAMAGE WAS NOTICED ELSEWHERE. BOLTS WERE RETORQUED IAW DHC-8 MM 27-32-41, PAGE 201. (M)

Part: BRACKET — CRACKED (LT CONTACTOR BOX)

DURING INSPECTION IT WAS NOTED THAT THE CIRCUIT BREAKER BRACKET HAD CRACKED ALLOWING THE CIRCUIT BREAKERS AND WIRING TO BECOME LOOSE IN THE AC CONTACTOR BOX. SUBMITTER STATES, THIS COULD CAUSE A SHORT CIRCUIT OF THE AFFECTED WIRING. A NEW BRACKET WAS FABRICATED AND INSTALLED ON FIELD AVIATION COMPANY WORK ORDER NR 21973.

Part: CONTROL CABLE — WORN (LT/RT AILERON)

DURING INSPECTION OF AIRCRAFT, FOUND THAT THE LEFT AND RIGHT WING AILERON LOWER CABLES WERE WORN BY PULLEY AT YW 400. CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORK ORDER NR 21973 AT C-CHECK.

Part: CONTROL CABLE — WORN (RT AILERON)

DURING INSPECTION OF AIRCRAFT IT WAS NOTED THAT THE RIGHT WING AILERON LOWER CABLE WAS WORN BY A PULLEY AT YW 190RT. CABLE WAS REPLACED ON FIELD AVIATION COMPANY WORK ORDER NR 21973 AT C-CHECK. (M)

Part: BRACKET — CRACKED (LT/RT MLG)

DURING INSPECTION OF AIRCRAFT IT WAS NOTED THAT THE LEFT AND RIGHT MLG RETRACTION SUPPORT BRACKETS APPEARED TO HAVE A FRETTING CONDITION. THE BRACKETS WERE REMOVED AND INSPECTED IAW AD CF 91-25R2. POSSIBLE CRACK INDICATIONS WERE VERIFIED BY MPI. IT SHOULD BE NOTED THAT THESE BRACKETS WERE PRE-MOD 8/2049 AND POST-MOD 8/1830 AND THAT MOD 8/1830 IS PART OF THE TERMINATING ACTION OF AD CF 91-25R2. BRACKETS WERE REPLACED PER MOD 8/2049 AND SB 8-54-34 ON FIELD AVIATION COMPANY WORK ORDER NR 21973.