N464AW

Part: CONTROL LEVER — FAULTED (FLAP SYS) · airframe 41,920 hrs · 40,896 cycles

FLAP FAIL AT 30 DEG WHEN SELECTING FLAPS DOWN. Ï¿½PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPPLEMENT 98-18IBOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED FLAP CONTROL LEVER IAW AMM SUPPLEMENT 09-038A, OPS CHECK GOOD, REMOVED PLACARD AND FROM MEL P/N:780501-3 S/N OFF:411A S/N ON:447A SKG

Part: SHUTOFF VALVE — FAULTED (RT A/C PACK) · airframe 41,701 hrs · 40,622 cycles

CLIMBING THROUGH 20000 FEET REV'D RT PACK OFF STATUS MESSAGE. LH PACK ON MEL. RT 10TH STAGE BLEED AIR VALVE INDICATE CLOSED IN COMMANDED OPEN POSITION. C/W QRH FOR UNPRESSURIZED FLIGHT. MESSAGE DID NOT CLEAR. DIVERTED TO MCI. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RH TEMP STAGE SOV IAW AWA SUP 19-036 OPS CHECK AND LEAK CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ACM) · airframe 41,674 hrs · 40,592 cycles

6170 - LEAVING TVC ON CLIMB OUT RH PACK HI PRESS CAUTION CAME ON REMAINED 2 SECONDS CREW DESCENDED 10K FT CW QRH RH PACK OPERATES NORMALLY. AIRCRAFT REMOVED FROM SERVICE. C/W INSPECTION OF RH PACK. FOUND TEMP HI PRESS CHECK IAW AMM 21-50-00. OPS CHECK GOOD AT THIS TIME.

Part: PROXIMITY SENSOR — FALSE INDICATION (MLG) · airframe 41,635 hrs · 40,542 cycles

GEAR DISAGREE WARNING MSG IN FLIGHT WITH LDG LEVER IN UP POS. MSG INTERMITTENT. GEAR INDICATION ON ED1 WAS LH, RH MAIN GEAR UP AND NOSE GEAR DOWN. C/W QRH MSG REMAINED CLEAR. AIRSPEED WAS 250 KTS WHILE ON APPROACH. AIRCRAFT REMOVED FROM SERVICE. PERFORMED GVI OF NLG, NO DEFECTS NOTED. CW M ACTION FOR MEL 32-30-01. REF 353097-2 FOR MEL. REPLACED THE PSEU PER AMM 32-61-01. GEAR SWINGS PER AMM 32-30. OPS CHECK GOOD. REMOVED PLACARD AND MEL.

Part: SENSOR — FAULTED (BRAKE POSITION) · airframe 41,655 hrs · 40,560 cycles

6172 - DESCENT IN CRUISE LEAVING FL260 FOR FL 240 RCVD FLAP FAIL CAUTION. FLAP LEVER NEVER TOUCHED. BTMS 6,7,7,6. DECLARED EMERGENCY. AIRCRAFT REMOVED FROM SERVICE. R&R RT BPSU IAM AMM 27-51-10-000-801 OPS CK GOOD

Part: PANEL — CRACKED (LT WING TE) · airframe 41,583 hrs · 40,478 cycles

LH WING TE PANEL AT WS 137.60 $ WS148.019 A SMALL CRACK WAS NOTED EMINATING FROM RIVET HOLE FROM A RIVET HOLE. AIRCRAFT REMOVED FROM SERVICE. REPAIRED IAW MHI REO 601R-57-21-3847 REV (--)

Part: FLAP SYSTEM — FAULTED · airframe 41,558 hrs · 40,450 cycles

FLAPS FAIL CAUTION IN CRUISE FAIL. FLAPS FAILED AT ZERO. RAN QRH PROCEDURE FOR FLAPS ZERO LANDING. NORMAL LANDING. AIRCRAFT REMOVED FROM SERVICE. IN WORK. PERFORMED RIGGING OF BPSU'S IAW AMM 27-51-10. FLAPS OPS CHECK GOOD AT THIS TIME. REMOVED PLACARD AND MEL

Part: SENSOR — FAULTED (TE FLAPS) · airframe 41,564 hrs · 40,461 cycles

FLAPS FAIL 6 DEG ON APPROACH ***** AIRCRAFT REMOVED FROM SERVICE ***** C/W FIM RESET PLACED ON MEL. R&R RH BPSU IAW AMM 27-51-10 AND SUPP 04-048B. OPS TEST GOOD. REMOVED PLACARD AND REMOVED FROM MEL.

Part: UNKNOWN — ODOR (CABIN) · airframe 41,121 hrs · 39,954 cycles

SMELL SIMILAR TO HOT METAL DETECTED IN FLIGHT DECK FOR ABOUT 10 SECS ROUGHLY 15 MIN APPLYING AC ELECTRICAL PWR TO AC REQ INSP. NO BREAKERS FOUND OPEN. APU WAS NOT OPERATING. NO SMOKE OR HAZE NOTED. AIRCRAFT REMOVED FROM SERVICE. INSPECTED COCKPIT AND AVIONICS BAY, CYCLED POWER SEVERAL TIMES IAW AMM 12-00-07 NO DEFECTS OR SMELLS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,924 hrs · 39,739 cycles

FLAP FAILED WHEN FLAPS SELECTED TO 20 DEGREE ON APPROACH. AIRCRAFT REMOVED FROM SERVICE REF 364863/1 FOR CORRECTIVE ACTION OPS CK GOOD IAW AMM 27-54-00 TROUBLESHOT FLAP FAIL PER FIM 27-50-00. REFERENCE FIM 27-50-00 FIG 103 BLK 21. OPS CK GOOD . REMOVED PLACARD AND REMOVED FROM MEL

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,926 hrs · 39,740 cycles

364863-1 FLAPS FAILED AT 0 DEGREES ON APPROACH WHEN SELECTING FLAPS 8. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT FLAP FAIL PER FIM 27-50-00. REFERENCE FIM 27-50-00 FIG 103 BLK 21. OPS CK GOOD . REMOVED PLACARD AND REMOVED FROM MEL

Part: POSITION SENSOR — UNKNOWN (FLAP SYSTEM) · airframe 40,234 hrs · 38,936 cycles

AFTER TAKEOFF FLAPS SELECTED ZERO AND SHORTLY THERAFTER RCVD FLAP FAIL CAU MSG. AIRCRAFT REMOVED FROM SERVICE. R&R OF BPSU ON RIGHT WING. OPS CHECK GOOD.

Part: CONTROL UNIT — UNKNOWN (FLAP SYS) · airframe 40,233 hrs · 38,935 cycles

FLAP FAIL CAUTION CLIMBING THROUGH 20,000FT. FLAPS INDICATE 0 DEGREES. AIRCRAFT REMOVED FROM SERVICE. R & R FECU IAW AMM 27-51-05 OPS CHECK GOOD AT THIS TIME.

Part: BULKHEAD WEB — DAMAGED (FS621) · airframe 39,999 hrs · 38,670 cycles

"Ï¿½REAR PRESSURE BULKHEAD FRAME STATION 621 DRILL START REVEALED AFTER REMOVAL OF FIRE BARRIER TOP FASTENER OTBD SIDE, FLAGGED. ***** AC REMOVED FROM SERVICE ***** REAR PRESSURE BULKHEAD STA. 621 REPAIRED IAW CRJ 200 REO 601R-61-7982 REV.-- DATED ON 31/ MAR/ 2023. "

Part: BEAM — CRACKED (FS559+16 TO FS55) · airframe 39,999 hrs · 38,670 cycles

BEAM 601R31119-60 CRACKED AT TOP AFT OUTBOARD CORNER LOCATED AT LBL9.00 BETWEEN FS559.00+16 AND FS559.00+32 *******AIRCRAFT REMOVED FROM SERVICE******* FABRICATED NEW BEAM AT LBL9.00 FS559.00+16 TO FS559.00+32 IAW DRAWING 601R31119 REV H. REMOVED AND REPLACED CRACKED BEAM WITH FABRICATED PART IAW CRJ200 SRM 51-42-06, 51-42-21 AND EA 105-2023-042 REV IR

Part: FLOOR SUPPORT — CORRODED (FS599 TO FS559.0) · corrosion level 2 · airframe 39,999 hrs · 38,670 cycles

AFT FUSELAGE INTERIOR, FLOORBOARD SUPPORT STRUCTURE CORRODED, 8" LEFT OF CTR LINE, 3" FWD OF FS 559+16 *********AIRCRAFT REMOVED FROM SERVICE************** REMOVED AND INSTALLED NEW FLOOR SUPPORT T. CAP FROM FS 559 TO 559+112 LBL 9.00 IAW CRJ 200 SRSM 51-40-11 AND EA 105-2023-042

Part: SEAT TRACK — CORRODED (CARGO FLOOR LH) · corrosion level 2 · airframe 39,999 hrs · 38,670 cycles

AFT FUSELAGE INTERIOR, FLOORBOARD SUPPORT STRUCTURE CORRODED FROM FS574 TO FS609 @ LBL27. REMOVED AND REPLACED FLOARBOARD SUPPORT STRUCTURE IAW EA# 105-2023-024 *******AIRCRAFT REMOVED FROM SERVICE*********** REMOVED AND REPLACED FLOARBOARD SUPPORT STRUCTURE IAW EA# 105-2023-024

Part: NONE — NONE · airframe 39,584 hrs · 38,285 cycles

GEAR DISAGREE ON TAKEOFF. LDG SELECTED UP. MSG RCVD AFTER 6 SEC. STEERING INOP AND NLG DOOR CAU MSG. NO HYD MSG. MANAUL RELESES SYS OPERATED. HYDS PUMP ON. EMER DECLARED. NLG REMAINED DOWN WHEN SELECTING GEAR UP. ****AIRCRAFT REMOVED FROM SERVICE**** SERVICED NLG IAW AMM 12-12-32. AND AWAC SUP 09-055. PERFORMED NLG EXTENSION AND RETRACTION. IAW AMM 32-30-00. OPS CHECK GOOD AT THIS TIME.

Part: COMPUTER — FAULTED (STALL WARNING) · airframe 38,400 hrs · 37,169 cycles

RECEIVED STALL CAUTION MESSAGE AFTER TAKEOFF CW QRH MESSAGE REMAINED, NO OTHER ASSOCIATED MESSAGES. FLAPS AND EICAS MATCHES FLAP POSITION COMMANDED AND GEARS COMMANDED UP IN TRANSITION. AIRCRAFT REMOVED FROM SERVICE. R & R STALL WARING COMPUTER IAW AMM 27-35-01 PERFORMED ADJUSTMENT TEST IAW AMM 27-35-01, FUNCTIONAL TEST PASSED, RESET MEMORY IAW AMM 27-35-01-820-801.

Part: FLOORBEAM — CORRODED (FS 559+59) · corrosion level 2 · airframe 37,939 hrs · 36,718 cycles

CORROSION DAMAGE AT AFT CABIN FLOOR SUPPORT AT FS559+59.5 AND RBL 9. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED FLOOR BEAM FLANGE REPAIR NO. 1 PER SRM 53-00-43 REV 38. P1 DAMAGE DIMENSION L= 1.900Ï¿½ X W= 0.700Ï¿½. CUT OUT DIMENSION L= 1.70Ï¿½ X W= 0.900Ï¿½. FABRICATED 1 REPAIR ANGLE, 1 REPAIR FLANGE, 2 FILLERS AND 1 RADIUS FILLER. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-53-51-603 REV (-) DATED 2021/09/18.

Part: SKIN — DENTED (FS 640) · airframe 37,939 hrs · 36,718 cycles

DENT ON AFT FUSELAGE SKIN FS640.00 TO FS644.5 AND S21R TO S22R. ***AIRCRAFT REMOVED FROM SERVICE*** DENT EVALUATED AND FOUND TO BE STRUCTURALLY ACCEPTABLE PER EA. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01680 REV IR DATED 9/13/2021.

Part: SKIN — DENTED (FS 625) · airframe 37,939 hrs · 36,718 cycles

DENT WITH CREASE ON AFT FUSELAGE SKIN AT FS625.00-FS640.0 AND S25R TO S26R. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR TO THE AFT FUSELAGE SKIN AT FS625.00-FS640.0 AND S25R TO S26R. DENT DIMENSION L = 1.100Ï¿½ X W = 0.600Ï¿½ X D = 0.013Ï¿½. CUTOUT DIMENSIONS L= 3.200Ï¿½ X W = 2.500Ï¿½. FABRICATED DOUBLER DIMENSIONS L = 9.500Ï¿½ X W = 8.750Ï¿½ FROM 0.063Ï¿½ CLAD ALUMINUM. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253-01679 REV IR DATED 9/13/2021.

Part: SKIN — DENTED (FS 625) · airframe 37,939 hrs · 36,718 cycles

AFT FUSELAGE SKIN HAS TWO DENTS AT FS625.30 TO FS640.0 AND S20L TO S21L, DENTS ARE APPROXIMATELY 1 INCH APART. ***AIRCRAFT REMOVED FROM SERVICE*** THE TWO DENTS EVALUATED AND FOUND TO BE STRUCTURALLY ACCEPTABLE PER EA. P/N 601R35005. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW ASAP EA # AWAC-CRJ253- 01681 REV IR DATED 9/14/2021.

Part: NONE — CRACKED (BULKHEAD) · airframe 37,939 hrs · 36,718 cycles

AFT PRESSURE BULKHEAD FS621 HAS INDICATION OF A CRACK AT BL 0.0 AND WL 125. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED INTERIM REPAIR TO AFT PRESSURE BULKHEAD FS621 AT BL 0.0 AND WL 125 TO WL134. PERFORMED DOUBLER REPAIR TO THE AFT PRESSURE BULKHEAD FS621.00 AT BL 0.0 AND 125 TO WL134. CUTOUT DIMENSIONS L= 8.100Ï¿½ X W = 1.700Ï¿½. FABRICATED DOUBLER DIMENSIONS L = 8.300Ï¿½ X W = 2.500Ï¿½ FROM 0.063Ï¿½ CLAD ALUMINUM AND TRIPLER FROM CLAD ALUMINUM 0.040Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW REO 601R-53-61-1285 REV E DATED 2016-10-31.

Part: DOUBLER — DENTED (FS 682) · airframe 37,939 hrs · 36,718 cycles

DENT ON AFT FUSELAGE SKIN AT FS682.00 TO FS700.00 AND S22R TO S23R FOUND NEXT TO AN AN EXISTING DOUBLER REPAIR WITH A DISTANCE OF 1.70Ï¿½ AWAY. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR TO THE AFT FUSELAGE SKIN BY REMOVING EXISTING DOUBLER AT FS682.00 - FS700 AND S21R TO S22R AND INSTALLED LARGER NEW DOUBLER AT FS682.00 TO FS700.00 AND S21R TO S23R. DENT DIMENSION L = 0.150Ï¿½ X W = 0.100Ï¿½ X D = 0.001Ï¿½. CUTOUT DIMENSIONS L= 17.00Ï¿½ X W = 4.800Ï¿½. FABRICATED DOUBLER DIMENSIONS L = 21.250Ï¿½ X W = 12.60Ï¿½ FROM 0.063Ï¿½ CLAD ALUMINUM. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW CRJ200 SRM 53-00-31 REV 38, SKIN-PLATING Ï¿½ REPAIR NO. 3 - EXTERNAL NON-FLUSH PERMANENT REPAIRS - NON PRESSURIZED AREA.

Part: SKIN — DENTED (FS 621) · airframe 37,939 hrs · 36,718 cycles

DENT ON AFT LOWER FUSELAGE SKIN DENT BELOW CARGO DOOR LOWER AFT CORNER FS621.00 AND S19L. ***AIRCRAFT REMOVED SERVICE*** PERFORMED A HAND DRESS TO FUSELAGE SKIN DENT BELOW CARGO DOOR LOWER AFT CORNER FS621.00 AND S19L. DENT DIMENSIONS PRIOR TO REWORK L= 2.95Ï¿½ X W= 0.250Ï¿½ X D= 0.030Ï¿½. POST REWORK DIMENSIONS L= 1.60Ï¿½ X W= 0.150Ï¿½ X D= 0.003Ï¿½. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WAS PERFORMED IAW MHIRJ REO 601R-53-61-7720 REV (-) DATED 2021/09/24.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 37,302 hrs · 36,050 cycles

RECEIVED LH ENG COWL A-ICE CAUTION MESSAGE IN FLIGHT WITH SYSTEM OFF. RAN QRH, MESSAGE CLEARED AFTER CLOSING LH 14TH STAGE SOV. LH PRESSURE RELIEF VALVE WAS FOUND TO BE OPEN ON THE GROUND. ***AIRCRAFT REMOVED FROM SERVICE*** R&R LH ENG COWL ANTI-ICE VALVE IAW AMM 30-22-01. RESET RELIEF VALVE IAW AMM 30-22-04. OPS CHECK OF BOTH GOOD. P/N:5399-00-1, S/N OFF:0182B, S/N ON:0692B. MPM

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 36,917 hrs · 35,630 cycles

DURING CLIMB FROM FL 280 WE HEARD A SOUND, SO WE CHECKED CABIN ALT, THAT WAS NORMAL. THE NOISE WAS GETTING LOUDER AND CABIN ALT SLOWLY INCREASED. AFTER DESCENDING THROUGH FL 250 RECEIVED CABIN ALT CAUTION FOLLOWED BY WARNING MESSAGE. CABIN O2 MASKS AUTO DEPLOYED. F/A REPORTS ALL PASSENGERS WERE USING THE O2 MASKS. AT 10,000 FT REMOVED MASKS IN COCKPIT AND SMELT AN ELECTRICAL/RUBBER KIND OF SMELL. SMELL CONTINUED UNTIL AFTER LANDING. CREW AND F/A COULD TELL THE NOISE WAS COMING FROM THE SERVICE DOOR AREA. F/A REPORTED NO SMELL UNTIL AFTER LANDING AND THEN IT CLEARED ON ITS OWN AFTER ABOUT 2 MIN. SYNOPTIC PAGE SHOWED NORMAL INDICATION ON ESC AND ELCT PAGES. NO DAMAGE NOTED ON WALK AROUND. AIRCRAFT REMOVED FROM SERVICE, REF WO 300163 FOR R & R OF BOTH CABIN PRESSURE CONTROLLERS. R & R OF CABIN PRESSURE SELECTOR PANEL AND R & R SERVICE DOOR SEAL.

Part: ANTENNA — FAILED (WX RADAR SYSTEM) · airframe 36,859 hrs · 35,566 cycles

"RADAR FAULT" MESSAGE ON MFD, RADAR MOSTLY INOP. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED WEATHER RADAR ANTENNA, PER AMM 34-41-01. OPS CHECK GOOD, PN 622-9302-003 S/N OFF 1WWH, S/N ON 3893 - LN.

Part: ACTUATOR — MALFUNCTIONED (RT MLG) · airframe 36,648 hrs · 35,356 cycles

UPON LDG EXTENSION, RECEIVED RT MLG INDICATION NOT DOWN WITH A GEAR DISAGREE AURAL WARNING. FOLLOWED QRH PROCEDURE, GEAR SHOWED DOWN AND LOCK AFTER 1 CYCLE OF THE GEAR LEVER. NO OTHER EICAS MESSAGES PRESENT, NO ABNORMAL HYD INDICATIONS NOTED. MANUAL RELEASE SYSTEM NOT OPERATED. INSTALLED DOWN LOCK SAFETY PINS IN MAIN AND NOSE LANDING GEAR AND REMOVED FLAGS FROM SAFETY PINS IAW AMM SUP 11-054 REF 306333/3 FOR MEL. R&R RT SIDE STAY ACTUATOR IAW AMM 32-32-01 OPS AND LEAK CHECK GOOD.

Part: TRANSMITTER — MALFUNCTIONED (LT WING TE FLAP) · airframe 36,191 hrs · 34,886 cycles

ON APPROACH WHEN SELECTING FLAPS TO LANDING CONFIGURATION (45 DEGREES) THE INDICATION STOPPED AT 42 DEGREES. THE CAPTAIN EXECUTED A GO A ROUND DUE TO THIS. AIRCRAFT REMOVED FROM SERVICE. C/W "M" ACTION TO DEACTIVATE LH FPTU IAW AMM 27-54-00-040-801. REF 318271/3 FOR MEL. PLACARDED AND PLACED ON MEL. REF 318271/4. FOR SKEW DETECTION MEL. R/R'D LH FLAP POSITION TRANSMITTER REF 27-55-01 S/N OFF: MULT3568343-001 S/N ON: MULT2906410-001

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 36,345 hrs · 35,038 cycles

INFLIGHT WHEN FLAPS WERE SELECTED TO 45 DEGREES, EICAS PAGE SHOWS FLAPS AT 42 DEGREES ON BOTH WINGS. NO CAUTION MESSGES. EXECUTED GO-AROUND, FLAPS RETRACTED NORMALLY, UPON EXTENSION BOTH FLAPS SHOW 42 DEGREES. AIRCRAFT REMOVED FROM SERVICE COMPLIED WITH FECU ADJUSTMENT TEST IAW AMM 27-51-05 FOUND ALL FLAP POSITION INDICATIONS NORMAL, OPS CHECKED GOOD, EICAS INDICATIONS NORMAL, INSPECTED FLAPS, NO DEFECTS.

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 35,553 hrs · 34,284 cycles

FS 605 FRAME BETWEEN STR 25R AND STR 25L HEAVY CORROSION WITH EXFOLIATION REMOVED AND REPLACED FRAME SECTION AND REINFORCEMENT ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 35,553 hrs · 34,284 cycles

FS 605 FRAME BETWEEN STR 25R AND STR 25L HAS HEAVY CORROSION WITH EXFOLIATION REMOVED AND REPLACED FRAME SECTION AND REINFOREMENT ANGLE IAW SRM 51-42-06 AND 51-42-21

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 35,553 hrs · 34,284 cycles

FS 605 FRAME BETWEEN STR 17R AND STR 18R HAS CORROSION REPAIR FRAME SECTION IAW REO 601R-53-61-7149

Part: ANGLE — CORRODED (BS 589) · corrosion level 2 · airframe 35,553 hrs · 34,284 cycles

ANGLE LOCATED AT FS 589 BETWEEN STRINGERS 22R AND 24R CORRODED. REPLACED

Part: FRAME — CORRODED (BS 589) · corrosion level 2 · airframe 35,553 hrs · 34,284 cycles

FS 589 FRAME BETWEEN STR 25R AND 25L AND BETWEEN STR 22R AND 21R HAS CORROSION. REPLACED

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 35,553 hrs · 34,284 cycles

RH WING I/B FLAP VANE LEADING EDGE IS CHAFED AT I/B SECTION REMOVED AND REPLACED RH WING IB FLAP VANE LEADING EDGE SKIN IB SECTION IAW CRJ 200 SRM 51-42-13

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 35,553 hrs · 34,284 cycles

RH WING INBD FLAP VANE LEADING EDGE IS CHAFFED AT CENTER SECTION. REPLACED

Part: BRACKET — CRACKED (BS 621 BULKHEAD) · airframe 35,553 hrs · 34,284 cycles

CRACKED LOWER ANGLE BRACKET ON 621 BULKHEAD REMOVED AND REPLACED LOWER ANGLE BRACKET IAW CRJ 200 SRM 51-42-21

Part: BEAM — GOUGED (CARGO DOOR) · airframe 35,553 hrs · 34,284 cycles

CARGO DOOR BEAM MEMBER HAS DEEP CUTS FWD AND AFT FROM THE CARGO DOOR PULLEYS REMOVED AND REPLACED CARGO DOOR BEAM MEMBER IAW CRJ 200 SRM 51-42-06

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · corrosion level 2 · airframe 35,553 hrs · 34,284 cycles

FLOOR BEAM CAP CORRODED IN AFT CARGO AREA, LBL 27 FS 559+80TI FS621.00. REPLACED BEAM CAP IAW REO 601R-53-00-027 REV-D.

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 33,553 hrs · 34,284 cycles

CARGO TRACK AT FS 559+78 TO FS 559+95 ON RBL 27 HAS CORROSION REMOVED AND REPLACED CARGO TRACK AT FS 559+78 TO FS 559+95 ON RBL27 IAW CRJ 200 AMM 53-00-49

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 35,553 hrs · 34,284 cycles

FLOOR BEAM CAP CORRODED AT RBL27, FS 559+80 TO 559+100. REPLACED BEAM CAP IAW REO 601R-53-00-027 REV-D,

Part: STIFFENER — CRACKED (BS 409) · airframe 35,553 hrs · 34,284 cycles

FS 409+128 BULKHEAD RBL 18 O/B POST IS CRACKED AT THE BOTTOM GOING APPROXIMATELY .200" PASSED THE BOTTOM RIVET REPAIR FS 409+128 BULKHEAD RBL 18 O/B POST IAW BOMBARDIER REO 601R-53-41-889 REV D.

Part: SEAT TRACK — CORRODED (BS 409-559) · corrosion level 2 · airframe 35,553 hrs · 34,284 cycles

LEFT FLOOR SEAT TRACK NR 3 CORRODED. REPLACED SEAT TRACK IAW 19-254A.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 35,553 hrs · 34,284 cycles

RIGHT FLOOR SEAT TRACK NR 4 CORRODED. REPLACED RIGHT FLOOR SEAT TRACK NR 4 IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (BS 399-409) · corrosion level 2 · airframe 35,553 hrs · 34,284 cycles

LEFT FLOOR SEAT TRACK NR 2 CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-11.

Part: FILLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,553 hrs · 34,284 cycles

LBL 27 FLOOR BEAM FITTING O/B AT F.S. 615 REPAIR FILLER HAS CORROSION REMOVED AND REPLACED DAMAGED FILLER AT LBL 27 FLOOR BEAM FITTING OUTBOARD AT FS 615 IAW STS EA 15-2013-417

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,553 hrs · 34,284 cycles

L/H OUTBOARD FLOOR SUPPORT ANGLE AT PAX DOOR ENTRY HAS CORROSION AT FS 333 TO FS 319.7, FLOOR LEVEL JUST ABOVE STRINGER 18L. REMOVED AND REPLACED ANGLE IAW CRJ-200 SRM 51-42-21 AND 51-42-06

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 35,553 hrs · 34,284 cycles

#4 FLOOR SEAT TRACK ON LBL 9 HAS CORROSION. REMOVED AND REPLACED #4 FLOOR SEAT TRACK ON LBL 9 IAW CRJ-200 AMM 53-01-01

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,553 hrs · 34,284 cycles

#1 FLOOR SEAT TRACK ON LBL 9 HAS CORROSION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,553 hrs · 34,284 cycles

FS 484 RBL 27 CLIP IS CRACKED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,553 hrs · 34,284 cycles

FS 484 LBL 27 OUTBOARD CLIP IS CRACKED AT THE TOP NEAR THE RADIUS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 35,553 hrs · 34,284 cycles

FS 280 LBL 9 INBD CLIP AT THE TOP OF THE RADIUS IS CRACKED. REPLACED.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 33,553 hrs · 34,284 cycles

CARGO DOOR SILL AT FS 605 INBD RIVET CRACKED. REPAIRED.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 33,553 hrs · 34,284 cycles

CARGO DOOR SILL AT FS 589 IS CRACKED AT INBD RIVET. REPAIRED.

Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 34,698 hrs · 33,484 cycles

3929 RECEIVED NWS INOP CAUTION MSG IN CRUISE. CW QRH MSG MOMNENTARILY CLEARED THEN RETURNED. CW FIM FASULT RESET MSG REMAINS. THE FLIGHT CREW FOLLOWED THE QRH, COORDINATED WITH ATC AND DISPATCH, DECLARED AN EMERGENCY, BRIEFED THE FLIGHT ATTENDANT AND PASSENGERS, CONTINUED TO DESTINATION AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TOWED TO THE GATE.

Part: FLAP — FAILED (WING) · airframe 34,337 hrs · 33,140 cycles

FLAPS FAILED AT ZERO DEGREES ON APPROACH.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 34,297 hrs · 33,098 cycles

FLAP FAIL CAUTION MESSAGE WHEN FLAPS SELECTED TO 30 DEGREES, FLAPS REMAINED AT 20 DEGREES, C/W QRH

Part: FLOOR SUPPORT — CORRODED (BS 559-564) · corrosion level 2 · airframe 32,020 hrs · 30,841 cycles

RIGHT FLOOR SUPPORT BETWEEN BS 559+85 TO 564 IS CORRODED.

Part: RISER — CRACKED (PAX DOOR) · airframe 32,020 hrs · 30,841 cycles

PAX DOOR AFT RISER PANEL CRACKED AT BOTTOM OF STEP. REPAIRED THE RISER.

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 32,020 hrs · 30,841 cycles

LBL 27, OTBD FLOOR SUPPORT BETWEEN BS 559+96 AND 559+112 HAS CORROSION AROUND FASTENER HOLES.

Part: PLATE — CORRODED (BS 559) · corrosion level 2 · airframe 32,020 hrs · 30,841 cycles

LIPPED PLATE COMMON TO THE RT FLOOR SUPPORT AT BS 559+86 IS CORRODED.

Part: ACCESS PANEL — CRACKED (PAX DOOR) · airframe 39,020 hrs · 30,841 cycles

PAX DOOR ACCESS PANEL CRACKED. REPLACED THE ACCESS PANEL IAW SRM 06-46-00.

Part: STRINGER — CRACKED (BS 379) · airframe 32,020 hrs · 30,841 cycles

STRINGER 3L JUST FWD OF BS 379 FOUND CRACKED.

Part: INTERCOSTAL — CRACKED (BS 621 BULKHEAD) · airframe 32,020 hrs · 30,841 cycles

AFT PRESSURE BULKHEAD INTERCOSTAL CRACKED AT BS 621, STRINGER 14L. REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 621 BULKHEAD) · airframe 32,020 hrs · 30,841 cycles

1014802-3000-0024 - APB INTERCOSTAL CRACKED AT FS 621.00 , STR 13L. REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21.

Part: ANGLE — CRACKED (BS 280) · airframe 32,020 hrs · 30,841 cycles

OTBD ANGLE ON STRINGER 3L IS CRACKED OTBD OF FRAME BS 280. REPLACED THE ANGLE IAW SRM 51-42-06, AND 51-42-21.

Part: BULKHEAD — CRACKED (BS 202) · airframe 32,020 hrs · 30,841 cycles

BS 202.75 BULKHEAD IS CRACKED AT LINE PASS THROUGH. REPAIRED THE BULKHEAD IAW REO 601R-53-11-563, REV C.

Part: SEAT TRACK — CORRODED (BS 409-559) · corrosion level 2 · airframe 32,020 hrs · 30,841 cycles

RIGHT SEAT TRACK CORRODED FROM BS 409+128 TO 559, RBL9. REPLACED THE SEAT TRACK IAW AMM 53-01-11, AND REO601R-53-00-485, REV-B.

Part: BRACKET — CRACKED (LT WING) · airframe 32,020 hrs · 30,841 cycles

LEFT WING LE CENTER OTBD ATTACH BRACKET IS CRACKED IN THE RADIUS.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,020 hrs · 30,841 cycles

AFT PRESSURE BULKHEAD IS CRACKED TA RBL 27 AND WL 81.5. PERFORMED REPAIR TO THE AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1285 REV-E.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 32,020 hrs · 30,841 cycles

FLOOR SUPPORT CRACKED AT BS 484, LBL 27. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06, AND 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 32,020 hrs · 30,841 cycles

CRACKED INTERCOSTAL AT FS 484.00, RBL27. REPLACED THE INTERCOSTAL IAW SRM 51-42-06, AND 51-42-21.

Part: SUPPORT BRACKET — CRACKED (BS 449) · airframe 32,020 hrs · 30,841 cycles

RIGHT SIDE OVER WING PANEL SUPPORT BRACKET CRACKED AT BS 449. REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06.

Part: SUPPORT BRACKET — CRACKED (BS 468) · airframe 32,020 hrs · 30,841 cycles

LEFT SIDE OVER WING PANEL SUPPORT BRACKET CRACKED AT BS 468. REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06.

Part: SUPPORT — CRACKED (BS 476) · airframe 32,020 hrs · 30,841 cycles

RIGHT SIDE OVERWING PANEL SUPPORT CRACKED AT BS 476. REPLACED THE SUPPORT IAW SRM 51-42-06, 51-40-11, 51-24-36, 51-21-11, 51-25-06, AND 51-25-16.

Part: SUPPORT BRACKET — CRACKED (BS 449) · airframe 32,020 hrs · 30,841 cycles

LEFT SIDE OVER WING PANEL SUPPORT BRACKET CRACKED AT BS 449. REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06.

Part: SUPPORT BRACKET — CRACKED (BS 461) · airframe 32,020 hrs · 30,841 cycles

RIGHT OVERWING PANEL SUPPORT BRACKET CRACKED AT BS 461. REPLACED THE SUPPORT BRACKET IAW SRM 51-42-06.

Part: SUPPORT — CRACKED (BS 468) · airframe 32,020 hrs · 30,841 cycles

RIGHT SIDE OVER WING PANEL SUPPORT BRACKET AT BS 468 CRACKED. REPLACED THE SUPPORT IAW SRM 51-42-06, 51-40-11, 51-24-36, 51-21-11, 51-25-06, AND 51-25-16.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 31,968 hrs · 30,789 cycles

STARTED APU ON APPROACH AND AFTER APU WAS RUNNING OBSERVED STRONG FUEL ODOR IN COCKPIT, TURNED OFF APU AND ODOR DISAPPAITED. RAN APU, NO FUEL, OR OIL LEAKS. OPERATED THE NR 1 PACK AND FOUND NO FUEL ODOR. SAME FOR THE NR 2 PACK. IAW AMM 21-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,151 hrs · 30,021 cycles

FLOOR EMERGENCY LIGHTS DO NOT ILLUMINATE BEYOND ROW 8. ADJUSTED THE LIGHT, OPS CHECKED GOOD IAW AMM 33-50-00

Part: ELECTRICAL SYS — ABNORMAL · airframe 29,412 hrs · 28,444 cycles

CREW REPORTED THAT WHEN THEY APPROACHED THE ACFT IT WAS CONNECTED TO GROUND POWER. CREW REPORTED THAT POWER WAS CYCLING ON & OFF UN-COMMANDED & THAT THEY COULD SMELL A BURNED ELECTRICAL ODOR.

Part: HOUSING — BROKEN (MAP LIGHT) · airframe 28,040 hrs · 27,147 cycles

CAPTAINS SIDE MAP LIGHT HOUSING IS BROKEN INTERNALLY, BURNING SMELL NOTED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,785 hrs · 26,900 cycles

FUSELAGE SKIN CRACKED, LBL 6 AFT CORNER OF NLG WW CUT OUT, REPAIRED.

Part: STIFFENER — CRACKED (RT EXHAUST) · airframe 27,784 hrs · 26,900 cycles

RIGHT EXHAUST NOZZLE FAIRING 446 AL HAS A CRACKED STIFFENER NEXT TO THE UPPER INBD MOUNT ASSEMBLY.

Part: DRAG ANGLE — CRACKED (PAX DOOR)

PASSENGER DOOR AFT DRAG ANGLE CRACKED AT PREVIOUS REPAIR ANGLE. R & R CRACKED PAX DOOR AFT DRAG ANGLE WITH NEW SERVICEABLE ANGLE PN 601R31772-5S IAW SRM 51-42-13 & 51-42-06.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 27,785 hrs · 26,900 cycles

WINDSHIELD CTR POST, LOWER LT ATTACH FITTING IS CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,784 hrs · 26,900 cycles

FS 589, LBL 45 CLIP UNDER CARGO DOOR TOP CRACKED, REPLACED.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 27,784 hrs · 26,900 cycles

FORWARD UPPER SUPPORT CHANNEL ON CARGO DOOR, FWD TRACK IS CRACKED. REPLACED CHANNEL.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 27,785 hrs · 26,900 cycles

WINDSHIELD CTR POST, LOWER RT ATTACH ANGLE, FITTING CRACKED. R & R FITTING.

Part: CONTROL CABLE — OUT OF POSITION (RUDDER) · airframe 27,784 hrs · 26,900 cycles

CO-PILOTS INBD RUDDER CABLE NOT IN RUN, OUTSIDE OF PULLEYS, AT APPROX FS 574, RBL 33 & CHAFING STRUCTURE. ACFT WAS IN HEAVY CHECK WHEN DISCREPANCY WAS DISCOVERED & STRUCTURE DAMAGE WAS LIMITED TO PAINT ONLY, SO PAINT WAS RESTORED. CABLE WAS REPOSITIONED, CABLE RUN VERIFICATION WAS PERFORMED & CABLE RIG & TENSION WAS ACCOMPLISHED.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,784 hrs · 26,900 cycles

SHOOT BOLT PLATE AFT OF FLOORBEAM 295 & INBD OF RBL 9 CORRODED, REPLACED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,784 hrs · 6,900 cycles

ANGLE CLIP IS CRACKED ON THE AFT SIDE OF FLOORBEAM 280 & INBD OF LBL 9. REPLACED ANGLE CLIP WITH NEW SERVICEABLE PART ON THE AFT SIDE OF FLOORBEAM 280 & INBD OF LBL 9 IAW SRM 51-42-21 & 51-42-06.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,784 hrs · 6,900 cycles

ANGLE CLIP IS CRACKED AT BEAM 280, OTBD SIDE OF RBL 9 IN CABIN. FABRICATED NEW ANGLE & INSTALLED AT FS 280, OTBD OF RBL 9 IAW SRM 51-42-06 & SRM 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,784 hrs · 26,900 cycles

ANGLE CLIP IS CRACKED AT BEAM 280, OTBD SIDE LBL9 IN CABIN. FABRICATED NEW ANGLE FOR LBL 9 OTBD TO FS 280 & INSTALLED IAW SRM 51-42-06 & SRM 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,784 hrs · 26,900 cycles

ANGLE CLIP IS CRACKED ON THE AFT SIDE OF FLOORBEAM 280 & INBD ON RBL 9. REPLACED ANGLE CLIP WITH NEW SERVICEABLE PART IAW SRM 51-42-21 & 51-42-06.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 27,784 hrs · 26,900 cycles

RIGHT WING CTR LE PANEL INBD ATTACH ANGLE AT TRANSITION, CRACKED IN LOWER RADIUS.

Part: ATTACH FITTING — CRACKED (COCKPIT) · airframe 27,785 hrs · 26,900 cycles

PILOT'S WINDSHIELD & SIDE WINDOW FRAME POST LOWER AFT ATTACH FITTING IS CRACKED.

Part: ATTACH FITTING — CRACKED (COCKPIT) · airframe 27,785 hrs · 26,900 cycles

CO-PILOT'S WINDSHIELD & SIDE WINDOW FRAME POST LOWER AFT ATTACH FITTING IS CRACKED.

Part: DOUBLER — SCRATCHED (FUSELAGE) · airframe 27,784 hrs · 26,900 cycles

FS 621 BULKHEAD FWD FACE, PREVIOUS REPAIR AT RBL 36, HAS SCRATCH MARKS FROM TRIM SCREWS. REMOVED PREVIOUS REPAIR. FABRICATED SERVICEABLE REPAIR DOUBLER 601R-53-61-1285-17 & INSTALLED IAW REO 601R-53-61-1285 REV D.

Part: DOUBLER — SCRATCHED (FUSELAGE) · airframe 27,784 hrs · 26,900 cycles

FS 621 BULKHEAD FWD FACE PREVIOUS REPAIR AT RBL 27, HAS SCRATCH MARKS FROM TRIM SCREWS. REMOVED PREVIOUS REPAIR. FABRICATED SERVICEABLE REPAIR DOUBLER 601R-53-61-1285-17 & INSTALLED IAW REO 601R-53-61-1285 REV D.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,784 hrs · 26,900 cycles

BEAM 280 UPPER ANGLE IS CRACKED JUST ABOVE ANGLE CLIP ON THE OTBD SIDE OF RBL 9 IN CABIN. REPAIRED ANGLE AT FS 280 BEAM IAW REO 601R-53-11-137 REV A.

Part: MOUNT BRACKET — CRACKED (RT MLG WW) · airframe 27,784 hrs · 26,900 cycles

RIGHT MLG BAY BRAKE PRESS SWITCH MOUNT BRACKET CRACKED. R & R RT MLG BRAKE TRANSDUCER BRACKET IAW SRM 51-42-06 & 51-40-11.

Part: MOUNT BRACKET — CRACKED (LT MLG WW) · airframe 27,784 hrs · 26,900 cycles

LEFT MLG BAY BRAKE PRESS SWITCH MOUNT BRACKET CRACKED. R & R TRANSDUCER BRACKET IAW SRM 51-42-06 & 51-40-11.

Part: DOUBLER — SCRATCHED (FUSELAGE) · airframe 27,784 hrs · 26,900 cycles

FS 621 BULKHEAD FWD FACE, PREVIOUS REPAIR AT LBL 27 HAS SCRATCH MARKS FROM TRIM SCREWS. REMOVED PREVIOUS REPAIR. FABRICATED SERVICEABLE REPAIR DOUBLER 601R-53-61-1285-17 & INSTALLED IAW REO 601R-53-61-1285 REV D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 27,785 hrs · 26,900 cycles

BATHTUB FITTING IS CRACKED AT FS 461, OTBD SIDE OF RBL 9.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,785 hrs · 26,900 cycles

LEFT FLOOR STRAP CORRODED OUT OF LIMITS AT FS 559, BETWEEN LBL 27 & LBL 36.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,029 hrs · 25,208 cycles

EMERGENCY FLOOR TRACK LIGHTING AT ROW 8 NOT WORKING.

Part: RETAINER — CORRODED (E/E BAY DOOR) · corrosion level 2 · airframe 23,020 hrs · 22,322 cycles

AVIONICS DOOR SEAL RETAINER HAS CORROSION. R & R AVIONICS DOOR SEAL RETAINER.

Part: DRAG ANGLE — CRACKED (UNKNOWN) · airframe 23,020 hrs · 22,322 cycles

CRACKED DRAG ANGLE. R & R DRAG ANGLE.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 23,020 hrs · 22,322 cycles

THREE CARGO TRACKS CORRODED ON LBL 27 BS 559+80, 559+112 & 621. BLENDED CORROSION, FOUND TO BE WITHIN LIMITS AT BS 559+80, & 621. FOUND TO BE OUT OF LIMITS AT BS 559+112, R & R CARGO TRACK.

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 23,020 hrs · 22,322 cycles

CARGO TRACK CORRODED ON RBL 9 AT BS 559+80 & 557+112. R & R CARGO TRACK IAW SRM 51-41-02, REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 53-21-49.

Part: RIB — CRACKED (LEFT) · airframe 23,020 hrs · 22,322 cycles

LEFT BATTERY RIB DRAG ANGLE IS CRACKED AT FWD RADIUS, REMOVED AND REPLACED.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 23,020 hrs · 22,322 cycles

LBL 27 IN CARGO BAY HAS CORROSION AT BS 621 TO 574. R & R FLOOR SUPPORT AND REPAIRED IAW EA 15-2013-417.

Part: TRUNNION — DAMAGED (MLG) · airframe 23,020 hrs · 22,322 cycles

DURING COLD WORK OF THE MLG TRUNNION LOWER FLANGES FOUND 1EA OVERSIZED HOLE ON LT SIDE. REPAIRED OVERSIZED HOLE IAW REO 601R-57-21-2000 REV -.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 23,020 hrs · 22,322 cycles

RIGHT INBD FLAP VANE CHAFED. REMOVED VANE AND FOUND TO BE WITHIN SERVICEABLE LIMITS. R & R INBD FLAP VANE IAW REO 601R-57-52-004, REV D.

Part: RIB — CRACKED (WING) · airframe 23,020 hrs · 22,322 cycles

LEFT BATTERY RIB IS CRACKED. REPAIR IAW REO 601R-57-51-046, REV B.

Part: SILL — CORRODED (BS 310-349) · corrosion level 2 · airframe 23,020 hrs · 22,322 cycles

PAX DOOR LOWER SILL CORRODED. R & R PAX DOOR SILL IAW SRM 51-42-06, 51-42-13 & 51-42-06.

Part: VANE — CHAFED (TE FLAP) · airframe 23,020 hrs · 22,322 cycles

INBD FLAP VANE IS CHAFED AT FLAP STATION 61,109 & 138. REPAIRED AND FOUND TO BE WITHIN LIMITS IAW REO 601R-57-52-004, REV D.

Part: ANGLE — CRACKED (BS 484) · airframe 23,020 hrs · 22,322 cycles

RT INBD AND OTBD FS 484 ANGLES CRACKED. REMOVEDAND REPLACED ANGLE.

Part: HINGE — CORRODED (DOOR STEP) · corrosion level 2 · airframe 23,020 hrs · 22,322 cycles

DOOR UPPER STEP HINGE HAS DEEP PITTING AND REQUIRES REPLACEMENT. INSTALLED SERVICEABLE IAW SRM 51-41-02.

Part: CARGO TRACK — CORRODED (BS 589-605) · airframe 23,020 hrs · 22,322 cycles

CARGO TRACK CORRODED AT FS 589-605. R & R CARGO TRACK WITH NEW SERVICEABLE TRACK IAW SRM 51-41-02.

Part: MOUNT — CRACKED (ASSIST MOTOR) · airframe 23,020 hrs · 22,322 cycles

PAX DOOR POWER ASSIST MOTOR MOUNT IS CRACKED. INSTALL SERVICEABLE REPLACEMENT.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 21,034 hrs · 20,416 cycles

DURING TAKEOFF & GEAR RETRACTION, "STEERING FAIL CAS MSG" & "NOSE GEAR DISAGREE" CAS MSG . COMPLIED WITH QRH. DISAGREE MESSAGE POSTED AT APPROX 5 SECONDS. GEAR WAS IN TRANSIT. GEAR SHOWED DOWN & LOCKED WHEN DEPLOYED. NO POSITIVE GEAR UP INDICATION DURING EVENT. REMOVED AND REPLACED NLG SELECTOR VALVE AND NLG PRIORITY VALVE PER AMM 32-33-10 AND AMM 32-32-15 OPS CHECK AND LEAK CHECK GOOD.

Part: SELECTOR VALVE — INOPERATIVE (MLG) · airframe 210,818 hrs · 20,398 cycles

GEAR DISAGREE WARNING & STEERING INOP CAUTION AFTER TAKEOFF. OCCURED ON RETRACTION WITH MESSAGE POSTED FOR 28 SECONDS DIVERTED & NORMAL LANDING. REPLACED NOSE WHEEL SELECTOR VALVE.

Part: STALL WARNING — INTERMITTENT · airframe 20,173 hrs · 19,572 cycles

STALL FAIL ON ROTATION- COMPLIED WITH QRH, RETURNED TO DEPARTURE, COMPLIED WITH FIM RESET PROCEDURES. NO DEFECTS NOTED AT THIS TIME. NOTED.

Part: WARNING MESSAGE — ILLUMINATED · airframe 19,939 hrs · 19,329 cycles

COOL CAUTION MESSAGE AFTER TAKEOFF, APROX 800 FT, COMPLIED WITH QRH, MESSAGE PERSISTED.

Part: TIRE — FAILED (MLG) · airframe 19,065 hrs · 18,466 cycles

RIGHT INBD TIRE SHREDDED. R & R NR 3 AND 4 MAIN TIRES IAW AMM 32-41-01,

Part: OIL SYSTEM — LOW (APU) · airframe 18,892 hrs · 18,280 cycles

APU FAULT CAUTION, APU AUTO SHUTDOWN, RESTARTED, RAN FOR 5 MIN, AUTO SHUTDOWN AGAIN RAN FOR 5 MIN AUTO SHUTDOWN AGAIN. INTERROGATED APU ECU SHUTDOWN HISTORY SHOWS SPEED LOSS. FOUND APU OIL LOW. SERVICED APU OIL WITH 2 QTS. OPS CHECKED IAW 49-10-00. OPS AND LEAK CHECKED GOOD.

Part: SEAL — FAILED (PAX DOOR) · airframe 18,145 hrs · 17,465 cycles

LOUD SQUEAL FROM MAIN CABIN DOOR IN FLIGHT. R & R PASSENGER DOOR SEAL IAW AMM 52-11-00. OPS CHECK GOOD.

Part: LEVER — CHAFED (PAX DOOR) · airframe 18,139 hrs · 17,460 cycles

PAX DOOR FWD PULL IN LOWER CHAFED. REPAIRED IAW REO 601R-52-11-504.

Part: BRACKET — BROKEN (WHEEL WELL) · airframe 18,139 hrs · 17,460 cycles

PRESSURE TRANSDUCER BRACKET IN LT WHEEL WELL BROKEN. REMOVED UNSERVICEABLE BRACKET AND REPLACED WITH SERVICEABLE BRACKET PN 601R75062-159 IAW SRM 51-42-06 AND SRM 51-42-22.

Part: FITTING — CHAFED (E/E DOOR) · airframe 18,139 hrs · 17,460 cycles

LT FWD DOOR FITTING CHAFED AT MAIN AVIONIC DOOR. BLENDED CHAFED AREA IAW REO 601R-53-21-1362 TREATED AREA IAW SRM 51-21-11, 51-25-06 AND SRM 51-25-16.

Part: SEAL — CHAFED (BS 559) · airframe 18,139 hrs · 17,460 cycles

RT SIDE OF FUSELAGE IS CHAFED AT RT INBD SEAL OF THE WING AND RT STUB FAIRING. REPAIRED CHAFED ARE ON RT SIDE OF FUSELAGE WHERE RT INBD SEAL OF THE WING AND RT STUB FAIRING MEET IAW REO 601R-53-41-610.

Part: ANGLE — WORN (FS 559.0) · airframe 18,139 hrs · 17,460 cycles

FS 559, LWR CAP ANGLE REQ`S REINFORCEMENT IAW REO 601R-53-41-116. LATEST REV IAW CUSTOMER REQUEST, REO 601R-53-41-116, REV B.

Part: STRUCTURE — CHAFED (RT WING TE FLAP) · airframe 18,139 hrs · 17,460 cycles

RT OTBD FLAP INBD EDGE IS CHAFED NEX TO THE ROLLER BLENDED CHAFED AREA IAW REO 601R5-57-53-847 TREATED AREA IAW SRM 51-21-14, SRM 51-25-06 AND SRM 51-25-16.

Part: SILL — GOUGED (BS 319.7-333) · airframe 18,139 hrs · 17,460 cycles

SERVICE DOOR CUT OUT GOUGED AT LOWER SILL FWD SIDE .240" LONG X .030" DEEP B/T FS 319.70 & 333.00. BLENDED DAMAGE TO DEPTH OF NO MORE THAN .030" IAW SRM 51-12-00.

Part: SEAT TRACK — CORRODED (FS559) · corrosion level 2 · airframe 18,139 hrs · 17,460 cycles

CORROSION CARGO FLOOR TRACK, LBL27-559+80. REMOVED UNSERVICEABLE TRACK PN 601R38779-9. LOCATED, DRILLED, INSTALLED SERVICEABLE TRACK N126-2075.

Part: COWLING — GOUGED (LT NACELLE) · airframe 18,139 hrs · 17,460 cycles

LT LOWER CORE COWL INNER SKIN GOUGED IN SPOTS. REPAIR IAW REO 601R-71-12-4077.

Part: HINGE — CHAFED (PAX DOOR) · airframe 18,139 hrs · 17,460 cycles

PAX DOOR HINGE HAS MINOR CHAFING ON 2 LUGS. REPAIRED DAMAGED PAX DOOR HINGE IAW REO 601R-52-11-1347.

Part: HINGE — CHAFED (PAX DOOR) · airframe 18,139 hrs · 17,460 cycles

PAX DOOR HINGE ON FUSELAGE HAWS CHAFING DAMAGE FROM ROLL PIN. REPAIRED CHAFED DAMAGE ON PAX DOOR HAING ON FUSELAGE IAW B/A REO 601R-52-21-814.

Part: BRACKET — CRACKED (WHEEL WELL) · airframe 18,139 hrs · 17,460 cycles

TWO BRACKETS FOR HYD LINES SYS 3 CRACKED IN RT WHEEL WELL LOCATED AND DRILLED BRACKETS IAW SRM 51-40-11. INSTALLED BRACKETS IAW SRM 51-41-02.

Part: PANEL — CRACKED (PAX DOOR) · airframe 18,139 hrs · 17,460 cycles

PAX DOOR FWD & AFT SIDE PANEL CRACKED AT STEPS 2 & 3. REPAIRED PAX DOOR FWD & AFT SIDE PANEL IAW REO 601R-52-11-702, REV C.

Part: RETAINER — DENTED (CARGO DOOR) · airframe 18,139 hrs · 17,460 cycles

CARGO BAY DOOR SEAL RETAINER DENTED ON LOWER AFT COMPARTMENT. R & R 2 EA SECTION OF CARGO DOOR SEAL REATINER IAW SRM 51-42-06.

Part: BULKHEAD — GOUGED (FS 280) · airframe 18,139 hrs · 17,460 cycles

BULKHEAD GOUGED 2 PLACES BEHIND GALLEY AREA. REPAIRED 2 EA GOUGES IAW REO 601R-53-11-1727, REV E.

Part: STRUCTURE — CHAFED (LT MLG DOOR) · airframe 18,139 hrs · 17,460 cycles

LT MLG DOOR CHAFED AT FWD AND AFT EDGES. REPAIRED DAMAGED AREAS OF LT MLG AT FWD AND AFT EDGES IAW REO 601R-52-82-106 AND 601R-52-82-102.

Part: SEAT TRACK — CORRODED (FS589) · corrosion level 2 · airframe 18,139 hrs · 17,460 cycles

CARGO FLOOR TRACK, LBL 9 AFT OF FS 589+80 HAS CORROSION. R & R SEAT (RAIL) TRACK AT LBL 9 AFT OF FS 589+80.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 18,139 hrs · 17,460 cycles

PAX DOOR AFT EDGE MEMBER CRACKED. REPAIRED PAX DOOR AFT EDGE MEMBER IAW REO 601R5211279.

Part: PLATE — CHAFED (PAX DOOR) · airframe 18,139 hrs · 17,460 cycles

PAX DOOR FWD & AFT STRIKER PLATES CHAFED. BLENDED OUT CHAFE.

Part: SEAT TRACK — CORRODED (FS 559) · corrosion level 2 · airframe 18,139 hrs · 17,460 cycles

CARGO FLOOR TRACK RBL 9 AFT OF FS 559+80 HAS CORROSION. R & R SEAT (RAIL) TRACK AT RBL 9 AFT OF FS 559+80.

Part: SKIN — DENTED (BS 684-703) · airframe 18,139 hrs · 17,460 cycles

ON RT SIDE OTBD OF AFT EQUIPMENT BAY OTBD OF DOOR ACFT HAS A DENT WITH A SCRATCH EXTENDING THRU DENT CUTOUT DAMAGED AREA ON RT OF OTBD OF AFT EQUIPMENT BAY OTBD OF DOOR REPAIRED ARE IAW REO 601R-53-00-023 BY INSTALLING PATCH/DOUBLER OVER DAMAGED AREA.

Part: RETAINER — CRACKED (NACELLE) · airframe 18,139 hrs · 17,460 cycles

PYLON PANEL 422AT HAS A CRACK IN THE SEAL RETAINER. REPLACED SEAL RETAINER.

Part: ANGLE — CRACKED (BS 621) · airframe 18,139 hrs · 17,460 cycles

LT OBLIQUE ANGLE CRACKED AT 621, PN 601-35012-51. R & R LT OBLIQUE ANGLE IAW REO 601R-53-61-422, REV NC.

Part: SEAL — CHAFED (BS 559) · airframe 18,139 hrs · 17,460 cycles

LT SIDE OF FUSELAGE IS CHAFED BY THE LT INBD SEAL OF THE WING AND THE LT STUB FAIRING COMPLIED WITH REO 601R-53-41-341.

Part: ANGLE — CRACKED (BS 621) · airframe 18,139 hrs · 17,460 cycles

RIGHT OBLIQUE ANGLE CRACKED AT 621 PN 601-35012-52. R & R RT OBLIQUE ANGLE IAW REO 601R-53-61-422, REV NC.

Part: RETAINER — CRACKED (PYLON) · airframe 18,139 hrs · 17,460 cycles

PYLON PANEL 422BT HAS A CRACK IN THE SEAL RETAINER. R & R SEAL RETAINER.

Part: DOUBLER — CRACKED (JET PIPE) · airframe 18,139 hrs · 17,460 cycles

RIGHT JET PIPE LOWER NUTPLATE DOUBLER IS CRACKED. REMOVED DAMAGED DOUBLER AND REPLACED WITH NEW.

Part: SHROUD — CHAFED (AILERON) · airframe 18,139 hrs · 17,460 cycles

INBD FIXED LOWER SHROUD ON RT AILERON IS CHAFED. BLENDED RT AILERON LOWER SHROUD IAW SRM 51-12-00 MAT LOSS .006, REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.

Part: SHROUD — CHAFED (RT AILERON) · airframe 18,139 hrs · 17,460 cycles

RT AILERON SHROUD PANEL 699AB IS CHAFED. BLENDED RT AILERON SHROUD PANEL 699AB IAW SRM 51-12-00 MAT LOSS, .007 REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW REO 601R5-57-60-020.

Part: SHROUD — CHAFED (RT AILERON) · airframe 18,139 hrs · 17,460 cycles

RT AILERON SHROUD PANEL 699BB IS CHAFED. BLENDED RT AILERON SHROUD PANEL 699BB IAW SRM 51-12-00 MAT LOSS, .009 REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.

Part: SHROUD — CHAFED (LT AILERON) · airframe 18,139 hrs · 17,460 cycles

INBD FIXED LOWER SHROUD ON LT AILERON IS CHAFED. BLENDED INBD LOWER SHROUD ON LT AILERON IAW SRM 51-12-00 MAT LOSS .008, REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.

Part: SKIN — CHAFED (WS 56.30) · airframe 18,139 hrs · 17,460 cycles

LEFT INBD FLAP VANE IS CHAFED. BLENDED LT INBD FLAP VANE, REMOVED .004 MAT, REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW SRM 51-12-00.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 18,139 hrs · 17,460 cycles

RT INBD FLAP VANE IS CHAFED IN 3 PLACES. BLENDED 3 PLACES ON LT INBD FLAP VANE REMOVED OF MAT REMAINING MAT IS WITHIN SERVICEABLE LIMITS IAW SRM 51-12-00.

Part: ACM — FAILED (LEFT) · airframe 17,961 hrs · 17,266 cycles

STRONG SULFUR/PLASTIC ODOR FROM PACK, AND LOUD WHINNING NOISE FROM REAR OF PLANE AT SAME TIME. CONFIRMED LT PACK ACM SEIZED, SEE 230117/4 FOR LT PACK MEL. R & R RT PACK PRSOV IAW AMM 21-51-43, RT PACK OPS CHECKED GOOD.

Part: ENGINE — FLAMED OUT (LEFT) · airframe 17,011 hrs · 16,243 cycles

AFTER 10,000 FT AND INCREASING TO CLIMB POWER, LEFT ENG ITT 854C, 62 DEGREE HIGHER THAN RT ENG ACARS`D MX, THEY REQUESTED CHECK WITH SPEED SWITCHES OFF, COMPLIED, NO DIFFERENCE NOTED REDUCED POWER, TURNED RT SPEED ON, NO DIFFERENCE. TURNED LT SPEED ON, ENGINE FLAMED OUT. C/W QRH, ENGINE START NORMAL. AFTER RESTART, LT ENG 80 DEGREES HOTTER THAN RT. ERFORMED BORESCOPE IAW AMM 71-00-00. FOUND UNSERVICEABLE DAMAGE TO STAGES 1, 2, AND 6 ON NR 1 ENG. R & R LT ENG. OK FOR SERVICE.

Part: IGNITION UNIT — INOPERATIVE (APU) · airframe 15,500 hrs · 14,637 cycles

APU WILL NOT START, START SEQUENCE NORMAL TO 25 PERCENT RPM, THEN RPM HANGS AND STRONG ODOR OF JET FUEL PRESENT. RAMP AGENTS REPORT SMOKE FROM APU EXHAUST. REPLACED APU IGNITION UNIT IAW AMM 49-41-01. OPS CK OF APU GOOD AT THIS TIME.

Part: APU — ODOR · airframe 14,684 hrs · 13,724 cycles

AFTER TRANSFERRING BLEEDS OT APU, SMOKE ENGULFED THE COCKPIT AND CABIN AREA, REQUEST INSP. FOUND ODOR TO BE PRESERVATIVE OIL USED IN APU. PERFORMED OPS CK OF LT/RT ACM`S. RAN ACM`S TO BURN RESIDUAL PRESERVATIVE OIL. NO ODOR NOTED AT THIS TIME.

Part: SEAL — FAILED (SERVICE DOOR) · airframe 13,417 hrs · 12,505 cycles

UPON CLIMBOUT, CABIN RATE CLIMB ABNORMALLY. ACFT NEVER PRESSURIZED CABIN ALT WAS 6700 FT AT 8000FT. C/W QRH SELECTED TO MANUAL PRESSURIZATION. ACFT DID NOT PRESSURIZE. REMOVED AND REPLACED SERV DOOR SEAL IAW 52-41-07. ALL WORK DONE ON W/O 140531. (K)

Part: SILL — CRACKED (BS 575) · airframe 13,398 hrs · 12,485 cycles

LT STGR 17 ON FLOOR SILL, QTY (X3) CRACK FOUND AROUND FASTENER HOLE OF RETAINING CLIP, DIMENSIONS ARE 0.100 TO .250 INCHES LONG. REPAIR AT FS 575.5 LT STGR 17 ON SILL FLOOR IAW REO 601R-53-61-1741. (K)

Part: LUG — GOUGED (RT MLG DOOR) · airframe 13,398 hrs · 12,485 cycles

RT MLG DOOR LUG HAS GOUGES DUE TO END ROD. RT MLG DOOR LUG REPAIRED IAW REO 601R-52-82-247. (K)

Part: FLOORBEAM — CORRODED (BS 280.00) · corrosion level 1 · airframe 13,398 hrs · 12,485 cycles

FWD ANGLE FLOORBEAM AT FS 280.00 CORRODED. FWD ANGLE FLOORBEAM AT FS 280.00 CORROSION REMOVED IAW SRM 51-21-06.

Part: LUG — DAMAGED (LT MLG DOOR) · airframe 13,398 hrs · 12,485 cycles

LT MLG DOOR LUG DAMAGED DUE TO WRONG HARDWARE INSTALLED ON ROD DOOR, LT MLG DOOR LUG REPAIRED IAW REO 601R-52-82-247 NC. (K)

Part: FRAME — CRACKED (BS 280) · airframe 13,398 hrs · 12,485 cycles

LT TOP FLANGE OF AFT ANGLE AT FS 280.00 CRACKED LT TOP FLANGE OF AFT ANGLE AT FS 280.00 CRACKED REPAIRED IAW REO 601R-53-11-138. (K)

Part: FRAME — CRACKED (BS 280) · airframe 13,398 hrs · 12,485 cycles

BOTTOM FLANGE OF FS 280.00 CRACKED AT LBL 9.0 BOTTOM FLANGE OF FS 280.00. REPAIRED IAW REO 601R-53-11-171 REV D. (K)

Part: FRAME — CRACKED (BS 280) · airframe 13,398 hrs · 12,485 cycles

RT BOTTOM FLANGE FS 280.00 AT RBL 9.0 CRACKED. BOTTOM FLANGE AT FS 280.00, RBL 9.0 CRACK REPAIRED IAW REO 601R-53-11-171, REV D. (K)

Part: STRUCTURE — CRACKED (BS 280) · airframe 13,398 hrs · 12,485 cycles

INBD AND OTBD OF RBL 9.0, CLIPS FS 280 CRACKED. INBD AND OTBD OF RBL 9.0, CLIPS FS 280.00, CRACKED REPLACED IAW SRM 51-42-06 AND 51-42-20. (K)

Part: ATTACH BRACKET — CRACKED (BS 718) · airframe 13,398 hrs · 12,485 cycles

RT HYDRAULIC MANIFOLD BRACKET AT FS 718.00 AFT AREA CRACKED. (.200") LONG. REO 601R-53-62-031, REV A. CARRIED OUT ON RT HYD MANIFOLD BRACKET AT FS 718.00. (K)

Part: STRUCTURE — CRACKED (BS 280) · airframe 13,398 hrs · 12,485 cycles

INBD AND OTBD OF LBL 9.0, CLIPS FS 280.00 CRACKED. INBD AND OTBD OF LBL 9.0, CLIPS FS 280.00, CRACKED REPLACED IAW SRM 51-42-06 AND 51-42-20. (K)

Part: LONGERON — CORRODED (BS 319-349) · corrosion level 1 · airframe 13,398 hrs · 12,485 cycles

CORROSION ON PAX DOOR LOWER SILL LONGERON. CORROSION ON PAX DOOR LOWER SILL LONGERON OTBD FACE REMOVED IAW SRM 51-21-06. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 13,398 hrs · 12,485 cycles

INTERCOSTAL AT FS 484.00, RBL 36 FOUND CRACKED (.25 LONG) INTERCOSTAL AT FS 484.00, FBL 36.00. REPAIRED IAW REO 601R-53-41-059, REV A. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 13,398 hrs · 12,485 cycles

INTERCOSTAL AT FS 484.00, LBL 36.00 FOUND CRACKED. INTERCOSTAL AT FS 484.00, LBL 36.00. REPAIRED IAW REO 601R-53-41-059, REV "A".

Part: SEAT TRACK — CORRODED (BS 364-690) · corrosion level 1 · airframe 13,398 hrs · 12,485 cycles

FLOOR SEAT TRACK BTW FS 364.00 AND FS 390.00, RBL 9.00 CORRODED. CORROSION ON FLOOR SEAT TRACK. (K)

Part: SEAT TRACK — CORRODED (BS 364) · corrosion level 1 · airframe 13,398 hrs · 12,485 cycles

FLOOR SEAT TRACK BTWN FS 364.00 AND FS 390.00, LBL 9.00 CORRODED. FLOOR SEAT TRACK CORROSION BTWN FS 364..00 AND FS 390.00, LBL 9.00. REMOVED IAW SRM 51-21-06 AND FOUND WITHIN LIMITS IAW SRM 53-21-49. (K)

Part: BULKHEAD — CRACKED (BS 621)

AFT PRESSURE BULKHEAD AT FS 621.00, LBL 27.50, WL 130.00 ABOVE CARGO DOOR TRACK FOUND CRACKED (.500 LENGTH). AFT PRESSURE BULKHEAD REPAIRED AT FS 621.00, LBL 27.50, WL 130 ABOVE CARGO DOOR TRACK CARRIED OUT IAW REO 601R-53-61-1541 REV "B".

Part: DOOR — LACK OF LUBE · airframe 12,999 hrs · 12,119 cycles

F/A REPORTS SERVICE DOOR DIFFICULT TO OPERATE. CLEANED AND LUBED SERV DOOR OPS CK NORMALLY IAW AMM 52-40-00. (K)

Part: UNKNOWN — UNKNOWN (IDG)

IDG NR2 CAUTION MESSAGE ON TAKEOFF AT 50 KNOTS. ABORTED TAKEOFF. BRAKE TEMP DIDN`T EXCEED 4. COMPLIED WITH IDG CAUTION QRH. DISCONNECTED IDG NR2. APU OIL LEVEL CHECKS GOOD IAW AMM 12-13-49, REF 187080/ 1 AND 2 FOR THE DIL AND MEL. LOG 187080/2 RECONNECTED IDG AND SERVICED IAW AMM 12-13-24, RAN ENG AND OPERATED IDG, OPS NORMAL AMM 24-20-00. (K)

Part: UNKNOWN — UNKNOWN (FLT CONTROLS) · airframe 11,939 hrs · 11,097 cycles

FLIGHT CONTROLS TAKE 2 TO 3 TIMES THE NORMAL AMOUNT OF PRESSURE TO MOVE SURFACE TO LIMITS WITH ALL HYD PUMPS ON. ONLY AILERONS AND ELEVATORS, RUDDER IS NORMAL, IN FLIGHT OR ON THE GROUND WITH AUTOPILOT OFF FROM BOTH CAPTS AND FO`S SIDE. C/W AWAC AMM SUP 2006-004A TEST OF PITCH FEEL SIMULATOR, AILERON AND ELEVATOR FORCES NORMAL. NO DEFECTS.

Part: CONNECTOR — LOOSE (RADIO ALTIMETER) · airframe 10,205 hrs · 9,432 cycles

GROUND LIFT DUMP AUTO DEPLOY ON ENGINE START. TIGHTENED RADIO ALTIMETER ANTENNA COAX CONNECTOR AND PERFORMED BONDING TEST PER AMM 51-80-00. SPOILER CONTROL SYSTEM OPS CHECK GOOD IAW AMM 27-65-00. RADIO ALTIMETER OPS CHECK GOOD IAW 34-44-01.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 9,708 hrs · 8,965 cycles

IN FLIGHT WHEN FLIGHT ATTENDANT TURNED ON COFFEE MAKER IT STARTED TO SMOKE. STOPPED SMOKING WHEN IT WAS TURNED OFF. REMOVED AND REPLACED COFFEE MAKER. (K)

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 9,274 hrs · 8,562 cycles

FLAPS FAIL MESSAGE ON APPROACH, FAILED AT 20 DEGREES WHEN SELECTING 30 DEGREES. RESET IAW SUPPLEMENT 98-018B. OPS CHECK NORMAL. (K)

Part: UNKNOWN — UNKNOWN · airframe 9,275 hrs · 8,563 cycles

ON TAKEOFF ROLL, AC VEERED RT, TOOK ALMOST FULL LT RUDDER TO STAY CENTERED ON RUNWAY. N1 SPEEDS WERE MATCHED. REDUCED POWER TO ABORT T/O AT 60 KNOTS. AIRCRAFT THEN TRAVELED STRAIGHT. BRAKE TEMPS WERE A 7 ON LT MAIN GEAR AND 3 AND 4 ON RT. WINDS 180 AT 5 KNOTS. (K)

Part: WARNING LIGHT — FALSE ACTIVATION

ON TAKEOFF ROLL, AIRCRAFT PULLED HARD LEFT, AT 10 KNOTS ABORTED. BRAKE TEMPS NORMAL 3, 3, 3, 3. AFTER REDUCING POWER TO IDLE RECEIVED CONFIG SPOILER MESSAGE. ENGINE POWER SETTINGS EQUAL. INSPECTED NLG TIRES AND MLG BRAKES 1 AND 2 PER AMM 32-40-00, NO FAULTS. TESTED NWS ECU PER AMM 32-50-00-240-801. NO FAULTS FOUND. FUNCTION CHECKED SPOILER CONTROL IAW AMM 27-61-00-720-801, NO FAULTS. (M)

Part: SUPPORT BEAM — CRACKED (BS 621)

FOUND CARGO DOOR TRACK SUPPORT BEAM ANGLE AT FS 621 IS CRACKED AT BOTTOM ANGLE. (M)

Part: ATTACH FITTING — CRACKED (BS 280)

FOUND FS 280 LBL 9 INBOARD AND OUTBOARD FLOOR SUPPORT CLIPS ARE CRACKED. 10-04-07 MAINTENANCE REPLACED CLIPS IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ 200 SRM 51-42-13 AND 51-42-21. (M)

Part: SKIN — CORRODED (LT WING)

THE LEFT WING LOWER PLANK ACCESS HOLE FOR PANEL 510AB AT WS 12.245 HAS PITTING APPROX .007 INCH DEEP. 10-04-07 MAINTENANCE C/W REPAIR OF LT WING LOWER PLANK ACCESS HOLE PANEL 510AB IAW REO 601R-57-20-030 REV F. (M)

Part: SKIN — CORRODED (RT WING)

THE RT WING LOWER PLANK ACCESS HOLE FOR PANEL 640BB HAS PITTING APPROX .005 INCH DEEP AT THE INBOARD AND OUTBOARD RADIUS. 10-04-07 MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)

Part: NUT CLIP — CRACKED (BS 280)

FOUND FS 280 RBL 9 INBOARD AND OUTBOARD FLOOR SUPPORT CLIPS ARE CRACKED. 10-04-07 MAINTENANCE REPLACED CLIPS IAW BSC STANDARD REPAIR 601R-53-0057A AND CRJ 200 SRM 51-42-13 AND 51-42-21. (M)

Part: SUPPORT BEAM — CRACKED (CARGO DOOR)

FOUND CARGO DOOR TRACK SUPPORT BEAM ANGLE AT FS 621 IS CRACKED AT BOTTOM ANGLE. MAINTENANCE REPLACED ANGLE IAW CRJ 200 SRM 51-42-21. (M)

Part: SKIN — CORRODED (LT WING)

THE LEFT WING LOWER PLANK ACCESS HOLE FOR PANEL 540BB AT WS 54.897 HAS PITTING APPROX .005 INCH DEEP AT THE INBOUND AND OUTBOARD RADIUS. 10-04-07 MAINTENANCE REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV F. (M)

Part: FLOORBEAM — CRACKED (BS 621)

FOUND LEFT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .3 INCH LONG. 10-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-61-117. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625)

LT FS 621-625 INTERCOSTAL ANGLE, P/N 601-35012-51, CRACKED APPROX .2 INCH LONG. 07-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-61-422 AND CRJ 200 SRM 51-42-06 AND 51-42-21. (M)

Part: FLOORBEAM — CRACKED (BS 484)

ANGLE CRACKED IN FLOOR SUPPORT STRUCTURE AT FS 484 LBL 27, WL 73.50. 10-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-41-059 AND BSC STANDARD REPAIR 601R-53-0029B. (M)

Part: FLOORBEAM — CRACKED (BS 621)

FOUND RIGHT FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .3 INCH LONG. 10-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-61-117. (M)

Part: FLOORBEAM — CRACKED (BS 484)

ANGLE CRACKED IN FLOOR SUPPORT STRUCTURE AT FS 484 RBL 27, WL 73.50. 10-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-41-059 AND BSC STANDARD REPAIR 601R-53-0029B. (M)

Part: INTERCOSTAL — CRACKED (BS 621-625)

FOUND RIGHT FS 621-625 INTERCOSTAL ANGLE, P/N 601-35012-52 CRACKED APPROX .2 INCH LONG. 10-04-07 MAINTENANCE REPLACED ANGLE IAW BOMBARDIER REO 601R-53-61-422 AND CRJ 200 SRM 51-42-06 AND 51-42-21. (M)

Part: CONNECTOR — UNKNOWN (NR 2 TEMP)

DURING FLIGHT , IDG NR 2 MESSAGE CAME ON AFT 28,000 FT, COMPLIED WITH QRH. AIR DIVERSION TO MDT, PERFORMED EMERGENCY LANDING. REMOVED AND REPLACED IDG NR 2, NO FIX. REMOVED AND REPLACED IDG NR 2 TEMP BULB, NO FIX. REMOVED AND REPLACED IDG HEAT EXCHANGER, NO FIX. REPLACED ENG IDG NR 2 TEMP CONNECTOR 2P22E2. OPS CHECK GOOD. IDG S/N 1110/3346 TSN 11659 CSN 10169 - IDG OIL COOLER S/N 1207 TSN 7641 CSN 6954. (M)

Part: FLAP — MALFUNCTIONED (T/E FLAP) · airframe 7,590 hrs · 6,909 cycles

FLAPS FAIL CAUTION WHILE IN FLIGHT, FAILED AT 30. COMPLIED WITH AWAC SUPPLEMENT 98-018A, NO FLAP TWISTING, SKEWING OR DEFORMATION NOTED. RESENT CIRCUIT BREAKERS ONCE, MESSAGE CLEARED. FLAPS OPERATE NORMALLY. PLACED ON 72 HOUR WATCH. (K)

Part: CONNECTOR — LOOSE (TE FLAPS)

FLAP FAIL MESSAGE DURING FLAP RETRACTION FROM 8 DEGREES TO 0 DEGREES, FLAP INDICATOR INDICATES 20 DEGREES. CHECKED FECU WHICH LED TO NR 1 OR LEFT BPSU. FOUND CONNECTOR TO BPSU LOOSE WITH MOISTURE INSIDE. CLEANED CONTRACTS AND RECONNECTED. REF 27-51-00, OPS CHECK GOOD. (M)

Part: WATER SEPARATOR — MALFUNCTIONED (CABIN)

WATER POOLING ON FLOOR BY 13C AND 13A, WATER APPEARS TO BE COMING FROM BEHIND CARPETED SIDEWALL PANEL. REPLACED RIGHT SIDE WATER SEPARATOR IAW AMM 21-51-13, OPS CHECK GOOD. (M)

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 4,385 hrs · 3,858 cycles

FLAPS FAILED AT 20 DEGREES ON APPROACH. NO DEFECTS NOTED. (K)

Part: STRUCTURE — DAMAGED (MLG WW)

WHILE RETRACTING RIGHT MLG DAMAGE OCCURRED TO THE UPLOCK APRON ASSEMBLY BY PUNCHING A HOLE APPROX 1.5 INCH BY 1 INCH. REPAIRED RIGHT MLG WHEEL WELL CHANNEL BY CUTTING OUT DAMAGE FABRICATING AND INSTALLING REPAIR IAW BRAS EO 601R-53-7036. (M)

Part: SKIN — CRACKED (FUSELAGE)

AIRCRAFT HAS EXTERNAL SKIN DAMAGE AROUND A/C POWER RECEPTACLE. (M)