N410AW

Part: SMOKE DETECTOR — FALSE ACTIVATION (ZONE 900) · airframe 48,243 hrs · 46,183 cycles

SMOKE TOILET CAUTION MESSAGE DISPLAYED WHILE PARKED AT GATE. C/W QRH MESSAGE REMAINED. C/B 2C5 2D14 2D15 2S2 2U2 PULLED. AIRCRAFT REMOVED FROM SERVICE. R&R LAV SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECK GOOD AT THIS TIME. CLOSED C/B 2C5, 2D14, 2D15, 2S2, 2U2. PN:PU90-421R3 SN OFF:08999 SN ON:07994

Part: WINGLET — DAMAGED (RIGHT WING) · airframe 47,227 hrs · 44,966 cycles

REPAIR TO RIGHT WINGLET TIP STRUCTURE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FOLLOWING ITEMS REF CRJ200 SRM 51-42-13, 51-40-11, 51-41-00, 51-42-06, 51-42-20, 51-42-13 REV.39. TIP FAIRING PN 600-15110-4; LEADING EDGE PN 600-15111-4; AFT FAIRING PN 600-15109-46; INBD STRAP PN 600-15108-16; OUTBOARD STRAP PN 600-15108-7; RIB PN 600-15116-12; INNER SKIN PN 600-15108-265; OUTBOARD SKIN PN 600-15108-245; SPAR REAR FWD PN 600-15104-10; RIB PN 600-15107-4; BRACKET PN 600-15103-4.IAW MHIRJ REO 601R-53-61-8143. REV Ï¿½ DATED 2024-03-06. HFEC ACCOMPLISHED, AND ALL FINISHES RESTORED IAW REO 601R-53-61-8143.

Part: SUPPORT BRACKET — CRACKED (POWER RECEPTICAL) · airframe 47,227 hrs · 44,966 cycles

CRACK FOUND ON POWER RECEPTACLE SUPPORT. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED BRACKET SUPPORT MEMBER P/N 600-33-83-33 ON POWER RECEPTACLE IAW SRM 51-42-06 REV. 39. ALL WORK PERFORMED UNDER WORK ORDER 004309, CARD 20031, TT: 47,227:03 TC: 44,966.

Part: FITTING — CRACKED (RH UPPER TRANS.) · airframe 47,227 hrs · 44,966 cycles

CRACKED FITTING ON UPPER TRANSLATING COWLING DOOR. ACFT REMOVED FROM SERVICE. REMOVED & REPLACED FITTING INTERLOCK RH ON UPPER TRANSLATING COWLING DOOR, IAW SRM 51-42-28 REV. 39 DATE 2024-05-08. ALL WORK PERFORMED UNDER WORK ORDER 004309. NO. 20124,

Part: SEAT TRACK — DAMAGED (BS 250-265 LBL12) · airframe 47,227 hrs · 44,966 cycles

REPAIR CAPTAINS I/B SEAT TRACK 601R-53-11-1093C. AIRCRAFT REMOVED FROM SERVICE. PERFORMED PERMANENT REPAIR ON FLOOR PANEL & ANGLE AT LBL 12 BETWEEN BS 250 TO 265 IAW MHI RJ REO 601R-53-11-3927 REV. -. ALL WORK PERFORMED UNDER WORK ORDER 004309, CARD 50008, HFEC ACCOMPLISHED & REPAIRED PROTECTIVE FINISHES.

Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 47,227 hrs · 44,966 cycles

AIRCRAFT REMOVED FROM SERVICE. REPAIR CAPTAINS I/B SEAT TRACK 601R-53-11-1093C. REPAIR CAPTAINS I/B SEAT TRACK 601R-53-11-1093C.

Part: CHANNEL — CORRODED (GALLEY FLOOR) · corrosion level 2 · airframe 47,227 hrs · 44,966 cycles

FWD GALLEY COMPARTMENT 112 LOWER STRIP HAS SIGNS OF CORROSION. ***** AIRCRAFT REMOVED FROM SERVICE ***** REPLACED LOWER STRIP ON FWD GALLEY COMPARTMENT 112 REF. C&D ZODIAC CMM 25-33-39 REV. 2

Part: DOUBLER — CORRODED (FWD FLOOR STRUCT) · corrosion level 2 · airframe 47,227 hrs · 44,966 cycles

RIGHT FWD GALLEY HARD POINT MOUNT CORROSION. ***** AIRCRAFT REMOVED FROM SERVICE ***** REPLACED RIGHT FORWARD GALLEY HARD MOUNT POINT REF. C&D ZODIAC CMM 25-31-56 REV. 8

Part: BRACKET — CORRODED (DOOR) · corrosion level 2 · airframe 47,227 hrs · 44,966 cycles

CORROSION FOUND ON SERVICE DOOR BASE STRUCTURE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BRACKET LOWER FRAM ON SERVICE DOOR BASE STRUCTURE IAW CRJ200SRM 51-42-20 REV39

Part: BLANKING PLATE — CRACKED (MLG WW) · airframe 47,227 hrs · 44,966 cycles

BLANKING PLATE IN LEFT AND RIGHT WHEEL WELL FOUND CRACKED ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED LH AND RH BRACKETS FROM WHEEL WELLS IAW CRJ200 SRM 51-42-06 REV 39.

Part: BRACKET — CORRODED (PAX DOOR FRAME) · corrosion level 2 · airframe 47,227 hrs · 44,966 cycles

CORROSION FOUND ON PASSENGER DOOR CUTOUT STRUCTURE IN 4 PLACES. FS319.7 TO FS349. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED 2 EA BRACKET ASSYS P/N 601R31527-217 ON PASSENGER DOOR SURROUND STRUCTURE AT FS310+5 AND FS 333+10 LBL 42 AND REMOVED AND REPLACED 1EA PLATE ON FLOOR STRUCTURE AT FS310 AND LBL36 IAW CRJ200 SRM51-42-06, 51-42-10, AND 51-24-21 REV 39.

Part: LINE — CRACKED (HYD SYSTEM) · airframe 47,227 hrs · 44,966 cycles

RH MLG HYDRAULIC LINE ANGLE SUPPORT BRACKET CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED 1EA BRACKET ASSY P/N 601R75262-153 ON RH MLG PANEL RACK AT FS 523.67 BETWEEN RBL18 AND RBL27 IAW CRJ200SRM 51-42-06 REV 39.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 47,227 hrs · 44,966 cycles

CARGO DOOR CROSSBEAM SUPPORT CRACKED ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED ANGLE P/N 601R35050-109 AT BAGGAGE DOOR ON AFT CARGO SURROUND STRUCTURE IAW CRJ200 SRM 51-42-21 REV 39.

Part: NONE — NONE · airframe 44,516 hrs · 42,134 cycles

AFTER T/O RECEIVED STEERING INOP CAUTION MSG. WT OFF WHEEL INOP CAUTION MSG. WT OFF WHEEL OUTPUT FAIL STATUS MSG. C/W QRH MSG PERSISTED. ***AIRCRAFT REMOVED FROM SERVICE*** R&R NLG RH WOW HARNESS PER CRJ 200 AMM 32-61-05 OPOS CK AND NLG STEERING GOOD PER CRJ 200 AMM 32-51-00. GEAR SWING GOOD GOOD PER CRJ 200 AMM 32-30-00

Part: NONE — NONE · airframe 43,981 hrs · 41,587 cycles

BOTH RIGHT MAIN LANDING GEAR TIRES WERE FLAT TAXING INTO GATE. ***AIRCRAFT REMOVED FROM SERVICE*** REF 343164/3, 343164/4, 343165/1, 343165/2, FOR THE CORRECTIVE ACTIONS, REPLACING #3 AND 4 MAIN TIRES

Part: PDU — MALFUNCTIONED (TE FLAPS) · airframe 43,134 hrs · 40,672 cycles

FLAPS FAIL CAUTION AFTER TAKE-OFF, FLAPS REMAINED AT 8 DEGREES WHEN SELECTING ZERO DEGREES (FLAPS FAILED AT 8 DEGREES), BRAKE TEMPS NORMAL ON LANDING. COMPLIED WITH FLAP RESET PROCEDURE IAW AWAC SUP. 98-18I, BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. AIRCRAFT REMOVED FROM SERVICE REF WO 303607 CARD 2 R/R PDU IAW AMM 27-52-01 OPS CHECK GOOD REMOVED FROM MEL AND REMOVED PLACARD LOG 322203\1: FLAPS FAIL CAUTION AFTER T.O. FLAPS REMAINED AT 8 DEGREES WHEN SELECTING ZERO. NOTE- FIM 27-50-00 FIG. 103 SPECIFIES PDU R+R AT BLOCK 13, PAGE 112.

Part: NUT — LOOSE (LT MLG WW) · airframe 42,274 hrs · 39,758 cycles

HYD 1 LO PRESS ON CLIMB-OUT, COMPLIED WITH QRH, RECEIVED HYD EDP 1A CAUTION. HYD 1B SELECTED ON APPROX. 1 MIN. SELECTED OFF PER QRH, HYD 1 LO PRESS RETURNED. NO OBSERVED TEMPERATURE CHANGE IN SYSTEM. "AIRCRAFT REMOVED FROM SERVICE" INSPECTED AND FOUND LOOSE AND LEAKING B NUT IN LEFT MAIN WHEEL BIN AREA. TIGHTENED B NUT AND OPS CHECK IN REF TO AMM 29-11-03 OPS CHECK GOOD NO LEAK NOTED. SERVICED HYD SYSTEM 1 IAW AMM 12-00

Part: PSEU — MALFUNCTIONED (E&E BAY) · airframe 42,267 hrs · 39,751 cycles

SHORTLY AFTER DEPARTURE OUT OF OKC, THE CREW RECEIVED A NOSE WHEELS STEERING INOP MESSAGE. THERE WAS A STEERING AND WOW INPUT CAUTION AT THE SAME TIME. THE FLIGHT AIR RETURNED TO OKC. NO OVERWEIGHT LANDING AND NO EMERGENCY WAS DECLARED "AIRCRAFT REMOVED FROM SERVICE" R&R PSEU IAW CRJ200 AMM 32-61-01 OPS CHECK GOOD PSEU IAW CRJ2OO AMM 32-61-00-720-801 PERFORMED 3 LANDING GEAR EXTENSION AND RETRACTION IAW CRJ 200 AMM 32-30-00-710-802 NO WOW INPUT AND STEERING MESSAGES DISPLAYED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,267 hrs · 39,751 cycles

SUPPLEMENTAL, STRINGER 26R CORRODED BETWEEN FS333 AND FS349. AIRCRAFT REMOVED FROM SERVICE: BLENDED TO REMOVE CORROSION. ORIGINAL MATERIAL THICKNESS - .080 MATERIAL LOSS - .080 REMAINING THICKNESS - 0.00 ALLOWABLE LIMITS - .008 REPAIRED STRINGER 26R IAW EA AWAC-CRJ253-01463 REV IR.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,267 hrs · 39,751 cycles

SUPPLEMENTAL, INTERCOSTAL JUST TO THE LEFT OF STRINGER 27 HAS CORROSION BETWEEN FS349 AND FS364. AIRCRAFT REMOVED FROM SERVICE. BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS - .080 MATERIAL LOSS - .010 REMAINING MATERIAL - .070 ALLOWABLE LIMITS - .008 REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-21 AND 51-42-06.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,267 hrs · 39,751 cycles

SUPPLEMENTAL, STRINGER 26L HAS CORROSION BETWEEN FS333 AND FS349. AIRCRAFT REMOVED FROM SERVICE. BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS - .063 MATERIAL LOSS - .030 REMAINING THICKNESS - .033 REMOVED AND REPLACED STRINGER SECTION IAW SRM 51-42-06 AND 53-00-03.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 42,267 hrs · 39,751 cycles

STRINGER 3 IS CRACKED AT FS379.00. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED STRINGER IAW CRJ200 SRM 51-42-06 & 51-42-21.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 42,267 hrs · 39,751 cycles

PAX DOOR LATCH COVER FWD ATTACH ANGLE IS CRACKED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED ANGLE IAW CRJ200 SRM 51-41-02.

Part: SPLICE ANGLE — CRACKED (FUSELAGE) · airframe 42,267 hrs · 39,751 cycles

FRAME SPLICE ANGLE AT FS 409+96 STRINGER 20 RIGHT IS CRACKED "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED CRACKED REINFORCING SPLICE ANGLE IAW CRJ 200 SRM 51-42-06 AND REO 601R-53-31-1092

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,267 hrs · 39,751 cycles

SERVICE DOOR LOWER SILL ANGLE CORRODED "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED SERVICE DOOR LOWER SILL ANGLE IAW CRJ 200 SRM 51-42-21

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,267 hrs · 39,751 cycles

RH #2 SEAT TRACK IS CORRODED. "AIRCRAFT REMOVED FROM SERVICE" BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS - .110 MATERIAL LOSS - .025 REMAINING THICKNESS .085 ALLOWABLE LOSS .020 REMOVED AND REPLACED SEAT TRACK IAW CRJ200 53-01-11.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 42,267 hrs · 39,751 cycles

SERVICE DOOR LOWER SILL ANGLE CORRODED "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED SERVICE DOOR LOWER SILL ANGLE IAW CRJ 200 SRM 51-42-21

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 42,267 hrs · 39,751 cycles

LEFT HAND #4 FLOOR SEAT TRACK CORRODED. "AIRCRAFT REMOVED FROM SERVICE" BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS - .110 MATERIAL REMOVED - .022 REMAINING MATERIAL - .088 ALLOWABLE LOSS - .011 REMOVED AND REPLACED SEAT TRACK IAW CRJ200 AMM 53-01-11

Part: SEAT TRACK — CORRODED (BS 409-559) · corrosion level 2 · airframe 42,267 hrs · 39,751 cycles

LH #3 FLOOR SEAT TRACK IS CORRODED. "AIRCRAFT REMOVED FROM SERVICE" BLENDED TO REMOVE CORROSION ORIGINAL THICKNESS - .110 MATERIAL LOSS - .022 REMAINING THICKNESS - .088 ALLOWABLE MATERIAL LOSS - .011 REMOVED AND REPLACED SEAT TRACK IAW CRJ200 AMM 53-01-11.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 42,267 hrs · 39,751 cycles

COMPLY WITH AWAC JOB CARD 4EOAWA21045-E17/003/453 MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS621.00 USING GREO 601R-53-61-1240 REV. D. "AIRCRAFT REMOVED FROM SERVICE" MODIFIED REAR PRESSURE BULKHEAD FS621 IAW GREO 601R-53-61-1240 REV. D.

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 42,267 hrs · 39,751 cycles

FLOOR BEAM IS CORRODED AT FS559+48 TO 559+80, RBL 9. "AIRCRAFT REMOVED FROM SERVICE" REPAIRED FLOOR BEAM IAW CRJ200 SRM 53-00-43, FIG. 203. BLENDED TO REMOVE CORROSION ORIGINAL MATERIAL - .050 MATERIAL LOSS - .024 REMAINING MATERIAL - .026 ALLOWABLE LOSS - .020

Part: SUPPORT — CRACKED (LT WING TE FLAP) · airframe 42,267 hrs · 39,751 cycles

LEFT INBOARD FLAP VANE, INBOARD END LEADING EDGE PANEL 584DT SUPPORT IS CRACKED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED SUPPORT IAW CRJ200 SRM 51-42-13

Part: SKIN — CHAFED (RT AILERON LE) · airframe 42,267 hrs · 39,751 cycles

RH AILERON UPPER LEADING EDGE SKIN IS CHAFFED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED LEADING EDGE SKIN IAW CRJ200 SRM 51-42-06 AND AWAC SUPPLEMENT 13-055B.

Part: ATTACH ANGLE — CRACKED (BS 621) · airframe 42,267 hrs · 39,751 cycles

LOWER ATTACH ANGLE ON AFT END OF BEAM IS CRACKED. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED ANGLE IAW CRJ200 SRM 51-42-21.

Part: SUPPORT ANGLE — CRACKED (BS 310) · airframe 42,267 hrs · 39,751 cycles

PAX DOOR UPPER LATCH CLOSE PLATE HAS A CRACKED SUPPORT ANGLE. "AIRCRAFT REMOVED FROM SERVICE" REMOVED AND REPLACED ANGLE IAW CRJ200 SRM 51-41-02.

Part: ANGLE — CRACKED (BS 625) · airframe 42,267 hrs · 39,751 cycles

FS625 TO INTERCOSTAL CLIP CRACKED AT STRINGER 14L. Ï¿½AIRCRAFT REMOVED FROM SERVICEÏ¿½ REMOVED AND REPLACED CLIP IAW CRJ200 SRM 51-42-21.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 42,267 hrs · 39,751 cycles

AFT PRESSURE BULKHEAD WEB IS CRACKED AT BL 0 AND WL 111.00. Ï¿½AIRCRAFT REMOVED FROM SERVICEÏ¿½ WORK TRANSFERRED TO AAR W.O. 1018176/2000/0019, S/N 7601432, C/W AWAC JOB CARD 4EOAWA21045-E17/003/453 - MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS621.00 USING BOMBARDIER GREO 601R-53-61-1240 REV. D.

Part: SUPPORT BRACKET — CRACKED (RT WING AILERON) · airframe 42,267 hrs · 39,751 cycles

RIGHT WING AILERON CENTER PANEL SUPPORT BRACKET IS CRACKED. Ï¿½AIRCRAFT REMOVED FROM SERVICEÏ¿½ REMOVED AND REPLACED SUPPORT BRACKET IAW CRJ200 SRM 51-42-06.

Part: DOOR SILL — CORRODED (BS 310-349) · corrosion level 2 · airframe 42,114 hrs · 39,600 cycles

PAX DOOR LOWER SILL ANGLE IS CORRODED. FULL LENGTH OF PART. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED LOWER SILL ANGLE I/A/W CRJ-200 SRM 51-42-06, 51-42-10, 51-42-21

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 42,267 hrs · 39,751 cycles

LEFT INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFFED IN TWO PLACES. AIRCRAFT REMOVED FROM SERVICE BLENDED TO SMOOTH CONTOUR FLAP STATION 56.50 MATERIAL LOSS .014 FLAP STATION 105.00 MATERIAL LOSS .026 ORIGINAL THICKNESS .050 REMOVED AND REPLACED LEADING EDGE SKIN IAW CRJ200 SRM 51-42-13

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 42,114 hrs · 39,600 cycles

CARGO SEAT TRACK AT LBL9, FS559.00+87 TO FS559.00+96 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE DAMAGE ORIGINAL THICKNESS .160 MATERIAL REMOVED .070 REMAINING MATERIAL .090 ALLOWABLE LOSS .060 REMOVED AND REPLACED TRACK IAW CRJ200 AMM 53-00-49.

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 42,114 hrs · 39,600 cycles

CARGO SEAT TRACK AT RBL9, FS559.00+87 TO FS559.00+96 IS CORRODED. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE DAMAGE ORIGINAL THICKNESS .160 MATERIAL LOSS .080 REMAINING THICKNESS .080 ALLOWABLE LOSS .060 REMOVED AND REPLACED TRACK IAW CRJ200 AMM 53-00-49

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 42,114 hrs · 39,600 cycles

PAX DOOR FLOOR SUPPORT CLEATS ARE CORRODED, FWD AND AFT. AIRCRAFT REMOVED FROM SERVICE BLENDED TO REMOVE CORROSION ORIGINAL MATERIAL .063 MATERIAL LOSS .018 REMAINING THICKNESS .045 ALLOWABLE LOSS .006 REMOVED AND REPLACED CLEAT AND BRACKET IAW CRJ200 SRM 51-40-11 & 51-42-06.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 42,267 hrs · 39,751 cycles

RIGHT WING IB FLAP VANE SKIN LE CHAFFED IN 3 PLACES. AIRCRAFT REMOVED FROM SERVICE BLENDED MID AND INBD AREAS IAW BOMBARDIER REO 601R-57-52-004 REMOVED AND REPLACED LE PANEL AT STA. 141 IAW CRJ200 SRM 51-42-13

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 42,114 hrs · 39,600 cycles

AFT PRESSURE BULKHEAD IS CRACKED AT CARGO DOOR AFT TRACK, APPROX. LBL27.5 AND WL 130. AIRCRAFT REMOVED FROM SERVICE REPAIR TRANSFERRED TO AAR W.O. 1018176/2000/0019 C/W AWAC JOB CARD 4EOAWA21045-E17/003/453 MODIFICATION OF THE REAR PRESSURE BULKHEAD WEB FS621 USING BOMBARDIER GREO 601R-53-61-1240 REV. D.

Part: SKIN — DENTED (FUSELAGE) · airframe 40,875 hrs · 38,449 cycles

EXTERNAL FUSELAGE SKIN IS DENTED BETWEEN FS 700.00 AND 736.00 AND BETWEEN STRINGER 16R AND 17R.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 40,870 hrs · 38,443 cycles

AT 600 FT AGL RECEIVED NLG UNSAFE (YELLOW CROSSHATCHED) ACCOMPLISHED G O AROUND AND CW QRH PROCEDURE. CYCLED GEAR AND RECEIVED 3 GREEN (INTER MITTENT) MC THIS INDICATION IS WITH GEAR DOWN ONLY AND INTERMITTENT. *FROM PLOT* - THE PILOT WAS ON APPROACH AND SELECTED GEAR DOWN. WHEN HE REACHED 600 FT, HE GOT A MSG THAT HIS NOSE GEAR WAS NOT GREEN, HE WENT AROUND, RAN THE QRH MANUAL, TURNED SYSTEM 3 HYDRAULIC PUMPS ON, CYCLED THE GEAR, HE GOT 3 GREEN, AND THEN LANDED.

Part: FRAME — CHAFED (FUSELAGE) · airframe 38,880 hrs · 36,517 cycles

REPAIR RT FRAME FS718.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 38,880 hrs · 36,517 cycles

PAX DOOR ASSIST MOTOR BRACKET CRACKED.

Part: DOUBLER — CRACKED (APU) · airframe 38,880 hrs · 36,517 cycles

APU OIL SERVICE DOOR HAS CRACK ON DOUBLER.

Part: SPOILER — DENTED (LT WING) · airframe 38,880 hrs · 36,517 cycles

MULTIPLE DENTS ON LT IB GROUND SPOILER.

Part: SPOILER — DENTED (LT WING) · airframe 38,880 hrs · 36,517 cycles

MULTIPLE DENTS ON LT OB GROUND SPOILER.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 38,880 hrs · 36,517 cycles

PAX DOOR AFT DRAG ANGLE CRACK BY ASSIST MOTOR YOKE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,880 hrs · 36,517 cycles

LT LOWER NOSE HYDRAULIC COMPARTMENT AFT UPPER LATCH CUT OUT SKIN IS CRACKED.

Part: STRUCTURE — CRACKED (APU BAY) · airframe 38,880 hrs · 36,517 cycles

APU ENCLOSURE HAS CRACK ON BACK SIDE.

Part: SKIN — NICKED (TE FLAP) · airframe 38,880 hrs · 36,517 cycles

LT I/B FLAP LOWER SKIN HAS MULTIPLE NICKS ON SKIN AND EXISTING REPAIR DOUBLER.

Part: BRACKET — CRACKED (LT WING) · airframe 38,880 hrs · 36,517 cycles

LEFT WING CENTER ANTI ICE TRANSITION BRACKET CRACKED AT FS 149.58. REPLACED BRACKET IAW SRM 51-41-02.

Part: BRACKET — CRACKED (RT WING) · airframe 38,880 hrs · 36,517 cycles

RIGHT WING FWD SPAR AT WS149.58 HAS A CRACKED TRANSITION BRACKET. REPLACED BRACKET IAW SRM 51-41-02.

Part: SKIN — DENTED (TE FLAP) · airframe 38,880 hrs · 36,517 cycles

LEFT INBOARD FLAP UPPER TRAILING EDGE SKIN HAS DENT AND DEFORMED EDGE. REPLACED TRAILING EDGE IAW SRM 51-42-13.

Part: SKIN — CHAFED (TE FLAP) · airframe 38,880 hrs · 36,517 cycles

LT O/B FLAP LEADING EDGE INBOARD END IS CHAFED. REPLACED LEADING EDGE IAW SRM 51-41-13.

Part: RIB — DAMAGED (TE FLAP) · airframe 38,880 hrs · 36,517 cycles

UPON REMOVAL OF LOWER FLAP SKIN ON LEFT I/B FLAP FOUND DAMAGED RIB PN: 601R14010-3. REPLACED RIB IAW SRM 51-42-06.

Part: RISER — CRACKED (PAX DOOR) · airframe 38,880 hrs · 36,517 cycles

PAX DOOR STEP RISER CRACKED ON LOWER SIDE. REPAIRED PAX DOOR STEP RISER IAW SUPP 13-134.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 38,880 hrs · 36,517 cycles

AC SERVICE PANEL ANGLE BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-41-02, 51-42-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,880 hrs · 36,517 cycles

RIGHT FLOOR SEAT TRACK NR 3 CORRODED FROM FS 409+128 TO 559.00, RBL9. REPLACED SEAT TRACK NR 3 RIGHT FLOOR IAW REO 601R-53-00-485 REV-D.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 38,880 hrs · 36,517 cycles

LT FLOOR SILL CRACKED AT FS 605.00, LBL42. REPAIRED SILL IAW REO601R-53-61-433 REV-C.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,880 hrs · 36,517 cycles

RIGHT FLOOR SEAT TRACK NR 4 CORRODED FROM FS 559.00 TO 559+80, RBL9. REPLACED RIGHT FLOOR SEAT TRACK NR 4 IAW SRM 51-21-06, 53-51-49 AND REO601R-53-00-485 REV-D.

Part: RETAINER — CRACKED (PYLON) · airframe 38,880 hrs · 36,517 cycles

PYLON PANEL 412BT HAD CRACKED SEAL RETAINER. REPAIRED SEAL RETAINER IAW SUPP 16-363.

Part: RETAINER — CRACKED (PYLON) · airframe 38,880 hrs · 36,517 cycles

PYLON PANEL 422BB HAS CRACKED SEAL RETAINER. REPAIRED SEAL RETAINER ON PNL 422BB IAW SUPP 16-363.

Part: RETAINER — CRACKED (PYLON) · airframe 38,880 hrs · 36,517 cycles

PYLON PANEL 412BB HAD CRACKED SEAL RETAINER. REPAIRED SEAL RETAINER IAW SUPP 16-363.

Part: WIRE HARNESS — UNSECURE (EMERGENCY LIGHTS) · airframe 38,621 hrs · 36,261 cycles

4203 EMERGENCY LIGHTS FROM ROW 10 REARWARD DO NOT LIGHT UP. RESECURED HARNESS AND OPS CHECK GOOD IAW AMM 25-60

Part: WIRE HARNESS — DAMAGED (NLG) · airframe 38,410 hrs · 36,040 cycles

AFTER TAKEOFF RECEIVED STEERING INOPATIVE CAUTION, WOW INPUT CAUTION, WOW OUTPUT FAIL STATUS MESSAGE, C/W QRH MESSAGE REMAIN. AFTER GEAR EXTENSION MESSAGE CLEARED. REMOVED AND REPLACED RIGHT SIDE NLG ELECTRICAL HARNESS IAW SUPP 12-029D, PERFORMED OPS CHECK, OPS CHECK GOOD. PERFORMED STEERING OPS CHECK, OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 38,183 hrs · 35,807 cycles

EMERGENCY LIGHTS INOPERATIVE BEYOND ROW 9. CONNECTED THE LIGHT CONNECTOR AT ROW 9 & OPS CHECKED IAW AMM 33-51-00, OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 30,833 hrs · 35,660 cycles

EMER LIGHT FLOOR ROWS 10-12 NOT WORKING. FOUND CONNECTOR AT ROW 12 LOOSE. RESECURED CONNECTOR EMER LIGHTS. OPS CHECKED GOOD. ALSO FOUND EMER LIGHT FLOOR COVER CRACKED FROM ROW 11-12. REMOVED AND REPLACED COVER PER AMM 33-51-01.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,850 hrs · 35,492 cycles

EMERGENCY LIGHTS AT ROWS 9-12 INOPERATIVE. INSPECTED AND FOUND BROKEN WIRE AT ROW 12. REMOVED AND REPLACED POWER SUPPLY CABLE IAW AMM 33-51-01 AND 16-371A. OPS CHECKED GOOD.

Part: FLAP SYSTEM — FAILED · airframe 37,740 hrs · 35,397 cycles

FLAPS FAILED AT ZERO DEGREES DURING CRUISE. PERFORMED FLAP ZERO NORMAL LANDING. PERFORMED FLAP RESET PROCEDURE IAW SUP 98-18G BOX 12. FLAPS RESET.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 37,243 hrs · 34,940 cycles

BURNING PLASTIC ODOR IN CABIN. BECAME STRONGER IN THE BACK OF THE AIRCRAFT. SMOKE ALARM DID NOT SOUND, NO ELECTRICAL SYSTEMS, LIGHTS, ALARMS APPEARED TO BE ERRATIC. SHUT DOWN ENTIRE AIRCRAFT PENDING MX CHECK. R & R BOTH LIGHT BALLASTS AT ROW 13A/C IAW AMM 13-095, OPS CHECKED GOOD, NO ODOR.

Part: UNKNOWN — ODOR (CABIN) · airframe 36,976 hrs · 34,685 cycles

MULTIPLE REPORTS OF OVERWHELMING FUEL ODOR IN CABIN. RAN ENGINES WITH CREW WITH BOTH PACKS ON, NO FUEL ODOR NOTED IN CABIN. INSPECTED AFT EQUIPMENT BAY, NO FUEL LEAKS NOTED NO OTHER LEAKS NOTED AS WELL IAW AMM 76-10-00

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 36,887 hrs · 34,608 cycles

FLOOR EMERGENCY LIGHTS ROW 9-12 INOPERATIVE. SECURED THE CONNECTOR AT ROW 9 IAW AMM 33-51-01. NO OTHER DEFECTS NOTED. OPS CHECKED GOOD.

Part: FLAP — MALFUNCTIONED (WING) · airframe 36,535 hrs · 34,285 cycles

FLAP FAIL CAUTION MSG AT CRUISE. C/W QRH PERFORMED FLAP RESET PROCEDURE IAW SUPPLEMENT 98-18G BOX 12 FLAPS RESET. PLACARDED AND PLACED ON MEL

Part: CONNECTOR — UNSECURE (SMOKE DETECTOR) · airframe 36,073 hrs · 33,840 cycles

SMOKE TOILET CAUTION MSG WITH INTERMITTENT SMOKE DETECTOR BEEP. ON GROUND TAXI WITH RT EMERGENCY ONLY AND BOTH PACKS ON. DURING INSPECTION OF LAV SMOKE DETECTOR FOUND CONNECTOR NOT SECURED. R & R SLIDE LATCH IAW ESPM 20-17-10. OPS CK GOOD IAW AMM 26-16-00 INSPECTED ACM'S CW AC PACK OPERATION, NO DEFECTS NOTED IAW AMM 21-51-00.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 36,013 hrs · 33,788 cycles

AFTER LANDING, SMOKE TOILET CAUTION MESSAGE ILLUMINATED FOR 20 SECONDS. SMOKE ALARM SOUNDED IN LAV. NO SMOKE PRESENT. REPLACED SMOKE DETECTOR.

Part: LIGHT — INOPERATIVE (ROWS 10-12) · airframe 35,535 hrs · 33,350 cycles

ROW 10 - 12 EMER LIGHTS INOPERATIVE.

Part: UNKNOWN — MALFUNCTIONED (FLIGHT CONTROL) · airframe 35,218 hrs · 33,069 cycles

FLIGHT 3882 CAPTAINS & FIRST OFFICERS YOKE REQUIRED EXCESSIVE FORCE TO TURN IN BOTH DIRECTIONS WITH AP ON & OFF, FLIGHT CONTROL SYNOPTIC PAGE SHOWED NORMAL, FLIGHT CONTROL CHECK PRIOR TO DEPARTURE NORMAL, HEAVY AFTER LANDING, NO ABNORMAL ISSUES WHEN AP SELECTED ON. REF TO WO 344943 FOR ALL MX CHECKS & INSPECTIONS & WORK PERFORMED. COULD NOT DUPLICATE DISCREPANCY ON GND. NO APPARENT DEFECTS NOTED AT THIS TIME.

Part: ANTI-ICE VALVE — MALFUNCTIONED (LT COWLING) · airframe 33,000 hrs · 32,997 cycles

WHILE IN CRUISE IN ICING CONDITIONS, UPON LEAVING ICING CONDITIONS, SELECTED WING & ENG ANTI-ICE OFF. RECEIVED LT COWL ANTI-ICE CAUTION MSG. COMPLIED WITH QRH DECLARED AN EMER. R & R LT COWL ANTI-ICE VLV IAW AMM 30-22-04. OPERATIONS CHECKED GOOD.

Part: NOT REPORTED — UNKNOWN (FLIGHT CONTROL) · airframe 35,050 hrs · 32,911 cycles

BOTH ELEVATOR & AILERON CONTROLS FEEL HEAVY IN FLIGHT ON BOTH SIDES, AUTOPILOT OFF.

Part: WEB — CRACKED (PAX DOOR) · airframe 34,905 hrs · 32,756 cycles

PASSENGER DOOR AFT WEB & PREVIOUS REPAIR CRACKED AT GAS SPRING MOUNT.

Part: POST — DAMAGED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

COMPLIED WITH REO 601R-53-41-1991 LATEST REVISION. FS 409+128, LBL 36, RBL 36, REPAIR OF VERTICAL POSTS & REPAIR OF PRESS BULKHEAD CAP ANGLE, REPAIRED.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 34,905 hrs · 32,756 cycles

PASSENGER DOOR UPPER AFT INTERCOSTAL CRACKED, REPLACED.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

VERTICAL BEAM STIFFENER ON THE FWD SIDE OF WING BOX AT LBL 27, FS 409+128, BOTTOM INBD SIDE IS CRACKED, REPAIRED.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

VERTICAL STIFFENER AT LBL 18, ON THE FWD SIDE OF WING BOX, AT FS 409+128. AT THE OTBD LOWER SIDE IS CRACKED, REPAIRED.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

VERTICAL BEAM STIFFENER ON THE FWD SIDE OF WING BOX, AT LBL 27, FS 409+128, BOTTOM OTBD SIDE IS CRACKED, REPAIRED.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

VERTICAL BEAM STIFFENER ON THE FWD SIDE OF WING BOX AT LBL 36, FS 409+128, BOTTOM INBD SIDE IS CRACKED, REPAIRED.

Part: STIFFENER — CRACKED (BS 409) · airframe 34,905 hrs · 32,756 cycles

VERTICAL STIFFENER AT RBL 27 ON THE FWD SIDE OF WING BOX, AT FS 409+123 IS CRACKED AT THE INBD LOWER SIDE IN THE FWD ECS COMPARTMENT, CRACK IS ABOUT 1.25" LONG.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,905 hrs · 32,756 cycles

STRINGER 27 HAS CORROSION, BETWEEN FRAMES 349.00 & 333.00 IN THE FWD E & E BAY. REPAIRED IAW SRM 53-00-13 & 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

SYSTEM 2 HYD RACK, AFT LOWER CORNER IS CRACKED. REPAIRED IAW 601R-53-62-031.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,905 hrs · 32,756 cycles

SEAT RAIL BEAM HAS CORROSION RBL 27, FS 574.00 - 621.00. REPAIRED RBL 27 SEAT RAIL BEAM CAP FROM FS 574.00 - 621.00 IAW REO 601R-53-00-005 REV B DATED 2011 01 06 & SRM 51-24-36, 51-42-06, 51-42-21, 51-21-11, 51-25-06, 51-25-16 & SUP 15-279.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,905 hrs · 32,756 cycles

FLOORBEAM LBL 27, OTBD PANEL LANDING HAS CORROSION, BETWEEN FS 559+112 - FS 621.00 IN THE CARGO BAY. REPLACED FLOORBEAM LBL 27, FS 559+112 - FS 621.00 IAW REO 601R-53-00-005 REV B DATED 2011 01 06, REO 601R-53-61-3778 REV A DATED 2011 07 15, SRM 51-42-06, 51-41-02, 51-40-11, 51-42-21, 51-24-36, 51-24-16, 51-21-11, 51-25-06 & 51-25-16.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

CENTER WINDSHIELD RT LOWER BRACKET CRACKED. R & R CTR WINDSHIELD POST BRACKET IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

SEAT RAIL BEAM AT FS 589 - 574, LBL 9, CORRODED, REPLACED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

FLOORBEAM AT STATION 280, RBL 13 CRACKED, REPLACED.

Part: BRACKET — CRACKED (COCKPIT) · airframe 34,905 hrs · 32,756 cycles

CENTER WINDSHIELD, LOWER LT POST BRACKET CRACKED, REPLACED.

Part: WEB — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

FORWARD E & E BAY, RT SIDE WEB CRACKED AT FS 193. REPAIRED FWD E & E BAY RT SIDE FLOOR IAW REO 601R-53-11-245 REV B.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

FLOOR ANGLE CLIPS, 4 CRACKED AT FS 280.00 & LBL 12. REPAIRED FLOORBEAM ANGLE CLIPS, 4 AT FS 280.00 & LBL 12 IAW REO 601R-53-11-136.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

VERTICAL FLOORBEAM ANGLES, 2 CRACKED FS 280.00, RBL 8. R & R VERTICAL FLOORBEAM ANGLES 2 AT FS 280.00, RBL 8, IAW REO 601R-53-11-171 REV D.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

VERTICAL FLOORBEAM ANGLE CRACKED AT FASTENER HOLES, FS 280.00 & LBL 8. R & R VERTICAL FLOORBEAM ANGLE AT FS 280.00 & LBL 8 IAW REO 601R-53-11-171.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

CLIP AT STRINGER 14L, INTERCOSTAL AFT SIDE OF FS 621.00, BULKHEAD IS CRACKED. R & R CLIP INTERCOSTAL AT FS 621.00, BULKHEAD & STRINGER 14L IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

ANGLE CLIP IS CRACKED ON THE OTBD SIDE OF LBL 9 AT FS 484, IN CABIN BELOW FLOOR. INSTALLED NEW ANGLE CLIP AT LBL 9 & FS 484 IAW SRM 51-42-06 & 51-42-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

CLIP AT STRINGER 13L, INTERCOSTAL AFT SIDE OF FS 621.00, BULKHEAD IS CRACKED. R & R CLIP INTERCOSTAL AT STRINGER 13L, ON AFT SIDE OF FS 621.00 BULKHEAD IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

ANGLE CLIP ON THE INBD SIDE OF RBL 36 AT FS 484 CRACKED, REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

WINDSHIELD POST ON CAPTAINS SIDE, AFT LOWER FITTING CRACKED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

WINDSHIELD POST ON FIRST OFFICERS SIDE, AFT LOWER FITTING CRACKED.

Part: STRAP — GOUGED (FUSELAGE) · airframe 34,905 hrs · 32,756 cycles

SEAL SURROUND AT FWD UPPER PIN FITTING ON L1 DOOR CUT OUT IS GOUGED.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,905 hrs · 32,756 cycles

FLOOR STRAP HAS CORROSION, BETWEEN RBL 36 & RT FLOOR SILL AT FS 559.00 IN THE CABIN. R & R FLOOR STRAP RBL 36 & FS 559.00 IAW SRM 51-42-06.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,905 hrs · 32,756 cycles

PASSENGER DOOR SILL AFT CLEAT CORRODED. REPAIRED PAX DOOR SILL AFT CLEAT IAW SRM 53-21-23, 53-00-00 & 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,905 hrs · 32,756 cycles

RIGHT FLOOR SEAT TRACK STICK 2 HAS CORROSION. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS. INSTALLED NEW SEAT TRACK IAW REO 601R-53-00-485.

Part: FUEL SYS — LEAKING (APU) · airframe 35,246 hrs · 41,987 cycles

AFTER START OF APU ON THE GND, STRONG FUEL ODOR FILLED THE CABIN, ODOR DISSIPATE UPON APU SHUTDOWN. INSPECTED AFT EQUIPMENT BAY & APU ENCLOSURE DRAINS, FOUND FUEL LEAKING FROM RT ENCLOSURE DRAIN WHILE APU PUMP IS ON. APU LEAK NOTED LEFT OF COMBUSTOR DRAIN ON COMBUSTION CASE, OIL IN APU, HAS FUEL CONTAMINATION. R & R APU ASSEMBLY IAW MX TASK CARD 00-49-310-01AW. OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 34,537 hrs · 32,403 cycles

ABORTED TO AT 55 KTS, DUE TO IDG 1 CAUTION. FOLLOWED BY GEN 1 CAUTION MSG.

Part: HYDRAULIC SYSTEM — FLUCTUATES (NR 1) · airframe 34,120 hrs · 31,988 cycles

FLIGHT 3987, HYD PUMP 2B PRESS FLUX 0-3000 PSI, UNUSUAL RUBBER & SMOKE ODOR. NO EVIDENCE OF RUBBER & SMOKE ODOR FROM THIS ACFT AT THIS TIME. HYD PRESS SYS NR 1 FLUX 0-3000 PSI, APPROX 1 TIME EACH 10 MIN.

Part: ENGINE — SURGES (LEFT) · airframe 34,082 hrs · 31,948 cycles

LEFT ENG ITT AT IDLE IS 590 DEGREES C & RT ENG ITT AT IDLE IS 480 DEGREES C. AT TAKEOFF POWER 91%, LT ENG WAS SLOW TO SPOOL UP, ITT IMMEDIATELY WENT TO 900 DEGREES C & AN AUDIBLE SURGE WAS HEARD FROM LT ENG. PERFORMED ENG POWER ASSURANCE CHECK IAW AMM 71-00-00-710-808. ALL CHECKED GOOD. ITT NORMAL, NO DEFECTS NOTED.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 34,032 hrs · 31,901 cycles

FLIGHT 3768, FLOOR TRACK LIGHTING AFT OF ROW 8 IS MISSING ARROWS. PLACARDED & PLACED ON MEL. R & R FLOOR TRACK LIGHTS AFT OF ROW 8 IAW AMM 33-51-01. OPERATIONS CHECKED GOOD. REMOVED PLACARD & REMOVED FROM MEL.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 33,511 hrs · 31,381 cycles

AFT PRESS BULKHEAD DAMAGED.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,184 hrs · 31,064 cycles

EMERGENCY LIGHTS ON RT SIDE WILL NOT ILLUMINATE. R & R AFT EMERGENCY LIGHT HARNESS IAW AMM 33-50. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,941 hrs · 30,837 cycles

LT WING EMERGENCY EXIT LOWER SIGN DOES NOT LIGHT UP. R & R NR 2 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,941 hrs · 30,837 cycles

EMERGENCY LIGHTS ROW 2 - 5, INOPERATIVE. R & R NR 2 INVERTER IAW AMM 33-51-07. OPS CHECKED GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 32,921 hrs · 30,814 cycles

3841 FLOOR EMER LIGHTS INOPERATIVE AT ROW 2 - 5. SECURED ELEC CONNECTOR AT ROW 3 IAW AMM 33-51-01 & SUPP 13-022. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 32,921 hrs · 30,814 cycles

EMERGENCY LIGHTS INOPERATIVE AT ROW 2 - 5. SECURED RED ELECTRICAL CONNECTOR AT ROW 3 IAW AMM 33-51-01 & SUPP 13-022. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,878 hrs · 30,770 cycles

SEVERAL SECTIONS OF FLOOR TRACK LIGHTING INOPERATIVE.

Part: LANDING GEAR — MALFUNCTIONED (MAIN) · airframe 33,002 hrs · 30,894 cycles

DURING GEAR RETRACTION ON TAKEOFF RECEIVED GEAR DISAGREE WARNING WITH NOSE GEAR INDICATING DOWN & BOTH MAINS UP. COMPLIED WITH QRH ALL 3 LANDING GEAR SHOWED DOWN. APPROX WT AT LANDING 47200. NOSE GEAR & NOSE DOOR MSGS. IN ADDITION, THE GEAR LEVER WAS LEFT IN THE UP POSITION & THE MANUAL RELEASE WAS PULLED IAW THE QRH. WERE IN SNOW BUT NOT SEVERE ICING, NO TURBULENCE OR SEVERE CONTROL MOVEMENTS. THE HYD Q, P & T WERE NORMAL IN ALL SYSTEMS. THE PUMPS WERE IN AUTO TILL TURNED TO ON IAW THE QRH, EMERGENCY LANDING WAS NOT DECLARED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 32,793 hrs · 30,694 cycles

ON DEPARTURE AFTER GEAR RETRACTION RECEIVED TRIPLE CHIME & NOSE GEAR DOOR WARNING MSG & GEAR DISAGREE MSG. RAN QRH & RETURNED. MSG POSTED IMMEDIATELY AFTER HANDLE MOVEMENT. HYD PUMPS WERE IN AUTO, NO OVERWEIGHT LANDING. MAINS SHOWED UP & LOCKED, NOSE GEAR SHOWED UNSAFE.

Part: CONNECTOR — OUT OF ADJUST (CABIN) · airframe 32,302 hrs · 30,216 cycles

3728 FLOOR LEVEL EMER LIGHTING INOPERATIVE BETWEEN ROWS 2 - 5. SIDEWALL EMER LIGHTS AT ROW 8AC INOPERATIVE. ADJUSTED EMER FLOOR LIGHT CONNECTION AT ROW 5. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 32,209 hrs · 30,127 cycles

AFTER DEPARTURE AT 3000 FT RECEIVED WING OVERHEAT WARNING MSG. COMPLIED WITH QRH MSG CLEARED WITH WING ANTI-ICE OFF, AIR RETURN TO CVG.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 32,200 hrs · 30,118 cycles

WING OVERHEAT WARNING MSG DURING CLIMB BETWEEN 5K & 8K FEET. IAW QRH TURNED OFF ANTI-ICE MSG EXT, USED STBY MODE FOR REMAINDER OF THE FLIGHT. MSG DID NOT RETURN.

Part: HINGE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 30,106 hrs · 28,131 cycles

PASSENGER DOOR TOP STEP HINGE CORRODED. REPLACED HINGE IAW CRJ200 SRM 51-41-02.

Part: SUPPORT — CRACKED (THRUST REVERSER) · airframe 30,106 hrs · 28,131 cycles

RIGHT TR NOSE COWL SUPPORT RING, SPRING SEAL, CRACKED OTBD LOWER POS 1. R & R WITH NEW SERVICEABLE SEAL IAW CMM 78-30-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 30,106 hrs · 28,131 cycles

FUSELAGE SKIN CRACKED IN AFT RT WW CUT OUT. REPAIRED IAW REO 601R-53-11-2614 REV.

Part: SKIN — GOUGED (FUSELAGE) · airframe 30,106 hrs · 28,131 cycles

LEFT FUSELAGE 3 INCH GOUGE DAMAGE AT FS 409.00 + 16 & WL 73.50. CUT OUT DAMAGE, FABRICATED & REPAIRED DOUBLER & FILLER, NDT CUT OUT, APPLIED CORROSION PREVENTION TREATMENT, PRIMER SURFACE TREATMENT, FAY & FILLET SEALED, INSTALLED REPAIR DOUBLER, FILLER & RESTORED TOP COAT.

Part: HANDLE — UNSERVICEABLE (CARGO DOOR) · airframe 30,106 hrs · 28,131 cycles

CARGO DOOR HANDLE HAS EXCESSIVE PLAY. REMOVED UNSERVICEABLE HANDLE ASSEMBLY & REPLACED WITH A NEW SERVICEABLE ASSEMBLY IAW CRJ 200 SRM 51-42-21 & SRM 51-40-11.

Part: TIE DOWN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,106 hrs · 28,131 cycles

CARGO FLOOR TIE DOWNS CLEATS AT FS 589 & 605 LBL 9 CORRODED. R & R IAW SRM 51-41-02.

Part: HOUSING — CHAFED (SERVICE DOOR) · airframe 30,106 hrs · 28,131 cycles

SERVICE DOOR OUTER HANDLE HOUSING IS CHAFED & GOUGED. REPLACED HOUSING IAW CRJ 200 SRM & AMM SRM 51-40-11 & SRM 51-42-21.

Part: SKIN PANEL — DAMAGED (TE FLAP) · airframe 30,106 hrs · 28,131 cycles

LIGHTNING BURN DAMAGE TO RT OTBD FLAP UPPER SKIN PANEL & TE. PERFORMED CHANNEL SPLICER & DOUBLER REPAIR IAW CRJ 200 SRM 57-53-00 REPAIR NR 3.

Part: MOUNT BRACKET — CRACKED (SERVICE DOOR) · airframe 30,106 hrs · 28,131 cycles

SERVICE DOOR INDICATOR SWITCH MOUNT IS CRACKED. R & R SWITCH MOUNT BRACKET WITH SERVICEABLE PART PN 601R38723-17 IAW CRJ SRM 51-40-11 & 51-42-21.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 30,106 hrs · 28,131 cycles

RIGHT BRAKE PRESS TRANSDUCER BRACKET IS CRACKED. R & R ONE EACH RT BRAKE PRESS TRANSDUCER BRACKET.

Part: MOUNT BRACKET — CRACKED (PAX DOOR) · airframe 30,106 hrs · 28,131 cycles

PASSENGER DOOR PRESS DOOR AFT MOUNT BRACKET CRACKED. REMOVED UNSERVICEABLE BRACKET, INNER ANGLE. FABRICATED & INSTALLED SERVICEABLE BRACKET, INNER ANGLE.

Part: VANE — CHAFED (TE FLAP) · airframe 30,106 hrs · 28,131 cycles

RIGHT INBD FLAP VANE IS CHAFED TWO SPOTS, INBD & MIDDLE LE SECTIONS, AT FLAP STATIONS 58 & 110. R & R UNSERVICEABLE SECTIONS OF RT INBD FLAP VANE LE WITH NEW SERVICEABLE LE SECTIONS.

Part: PLATE — CRACKED (FUSELAGE) · airframe 30,106 hrs · 28,131 cycles

CARGO THRESHOLD STEP PLATE CRACKED. STOP DRILLED & REMOVED CRACK DAMAGE IAW CRJ 200 SRM 51-12-00.

Part: ACOUSTIC PANEL — DAMAGED (RT TRANS COWL) · airframe 30,106 hrs · 28,131 cycles

RIGHT LOWER TRANS COWL ACOUSTIC PANEL HAS FIVE EACH DENTS WITH GOUGING & CRACKED SKIN. REPLACED FIVE DENTS IAW CRJ 200 SRM 51-12-00. REPAIRED WITHIN STRUCTURAL LIMITS, NO CRACKS NOTED IN SKIN.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 30,106 hrs · 28,131 cycles

RIGHT WING INBD LE PANEL OTBD ATTACH ANGLE CRACKED AT LOWER RADIUS. R & R ATTACH ANGLE.

Part: MOUNT — CRACKED (FUSELAGE) · airframe 30,106 hrs · 28,131 cycles

STATION 574 FWD LATCH MOUNT AT CARGO DOOR, CRACKED UNDER FASTENERS, FOUR EACH THAT ATTACH MOUNT TO SILL. SMALL CRACKS AROUND FASTENER HOLES. REPAIRED IAW REO 601R-53-61-1741 WITH A DOUBLER & PACKER.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 30,106 hrs · 28,131 cycles

PASSENGER DOOR UPPER LINTLE ATTACH ANGLES AT FS 280 BULKHEAD CRACKED. R & R UPPER LINTLE ATTACH ANGLES.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,106 hrs · 28,131 cycles

LEFT UPPER OBLIQUE ANGLE IS CRACKED AT FS 621. R & R IAW SRM.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 30,106 hrs · 28,131 cycles

BRAKE PRESS TRANSDUCER BRACKET LT WW CRACKED. REMOVED CRACKED BRACKET & INSTALLED NEW SERVICEABLE BRACKET IAW CRJ SRM 51-42-06, 50-40-11.

Part: DRAG ANGLE — CRACKED (LT MLG WW) · airframe 30,106 hrs · 28,131 cycles

LEFT WW DRAG ANGLE CRACKED. R & R IAW CRJ 200 SRM 51-42-21.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 30,106 hrs · 28,131 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. REMOVED UNSERVICEABLE DRAG ANGLE & TWO EACH CLIPS & REPLACED WITH SERVICEABLE DRAG ANGLE & TWO EACH CLIPS.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,106 hrs · 28,131 cycles

RIGHT UPPER OBLIQUE ANGLES CRACKED AT FS 621. R & R IAW SRM.

Part: DRAG ANGLE — CRACKED (RT MLG WW) · airframe 30,106 hrs · 28,131 cycles

RIGHT WW DRAG ANGLE CRACKED. R & R IAW SRM.

Part: SUPPORT FITTING — CRACKED (PAX DOOR) · airframe 30,106 hrs · 28,131 cycles

PASSENGER DOOR CLOSING PLATE SUPPORT CLIP NR 3 IS CRACKED. REMOVED, FABRICATED & REPLACED.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 30,106 hrs · 28,131 cycles

UNDERFLOOR SUPPORT AT RBL 28 & FS 484 HAS INBD ATTACH CLIP CRACKED. REMOVED UNSERVICEABLE FS 484 CLIP IAW CRJ 200 SRM 51-42-06 & 51-42-21. INSTALLED A SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-06 & 51-42-21 & REO 601R-53-41-059 REV B.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,106 hrs · 28,131 cycles

CARGO FLOOR SEAT TRACK ON LBL 27 CORRODED FROM FS 559+122 & 559+96. R & R CORRODED SEAT TRACK IAW AMM 53-01-11.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 30,106 hrs · 28,131 cycles

FUSELAGE STATION 484 & LBL 28 FLOOR SUPPORT ANGLE ATTACH CLIP IS CRACKED. REMOVED CRACKED CLIP & REPLACED WITH NEW SERVICEABLE CLIP.

Part: CARGO TRACK — CORRODED (CAARGO BAY) · corrosion level 2 · airframe 30,106 hrs · 28,131 cycles

CARGO FLOOR TRACK ON LBL 27 CORRODED FROM FS 559+112 - 559+96. R & R CORRODED SEAT TRACK IAW AMM 53-01-11.

Part: RECEPTACLE — BURNED (EXTERNAL POWER) · airframe 30,027 hrs · 28,057 cycles

EXTERIOR PWR RECEPTACLE DAMAGED, SHOWS SIGNS OF BURNS. PLACARDED & PLACED ON MEL. MC IAW AMM & ORF MX CONFIRMED THIS, ADG MUST BE DROPPED TO ACCESS WIRING ON BACK SIDE OF PLUG TO REPLACE IT. R & R EXT PWR RECEPTACLE IAW AMM 24-41-03, OPERATIONS CHECKED GOOD. NO OTHER DAMAGE NOTED. ACFT SYS CHECKED GOOD REMOVED PLACARD & FROM MEL.

Part: WARNING MESSAGE — ILLUMINATED (LANDING GEAR) · airframe 29,750 hrs · 27,796 cycles

AFTER TO RECEIVED WARNING GEAR DISAGREE AND NOSE DOOR OPEN AND CAUTION MESSAGES WOW INPUT AND STEERING INOP NAD STATUS MESSAGE WOW OUTPUT FAIL NOSE GEAR WAS GREEN DOWN. MAINS WERE UP AND WHITE. RAN QRH. ON GEAR EXTENSION ALL MESSAGES CLEARED EXCEPT WOW INPUT AND STEERING INOPERATIVE CAUTION.

Part: STRUT — DISCHARGED (NLG) · airframe 29,750 hrs · 27,796 cycles

NOSE GEAR FAILED TO RETRACT ON SELECTION. FOUND NLG TO BE UNDER SERVICED WITH NITROGEN. STRUT ON LT SHOWED 3 INCHES OF CHROME. NO EVIDENCE OF LEAKS. SERVICED NLG WITH NITROGEN IAW AMM 12-12-32, LEAK AND OPS CHECKED GOOD.

Part: STRUT — DISCHARGED (NLG) · airframe 29,489 hrs · 27,536 cycles

GEAR DISAGREE WARNING AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT, RAN QRH, RETURNED TO FIELD. SERVICED NLG STRUT TO LIMITS ALLOWING PROPPER DEPT OF NLG OLEO. EXTENSION PROXIMITY SENSOR PERFORMED MULTIPLE GEAR SWING. OP CHECKED GOOD, NO FLUID LEAKS NOTED.

Part: SKIN — SCRATCHED (BS 718-759) · airframe 29,328 hrs · 27,384 cycles

DAMAGE, REF 240056-1, AFT FUSELAGE LOWER SKIN SCRATCHED FROM AEB DOOR TOWARD TAIL. REPAIR IAW STS EA 15-2013-377 & IN LIMITS 718-734.

Part: AHRS — FAILED (NR 2) · airframe 28,980 hrs · 27,043 cycles

DURING CRUISE AND ON FINAL APPROACH. EXPERIENCED UNCOMMANDED RUDDER MOVEMENT. RUDDER FLUTTER. DID NOT TURN OF YAW DAMPENER. R & R NR 2 AHRS.

Part: AHRS — MALFUNCTIONED (NR 2) · airframe 28,980 hrs · 27,043 cycles

IN CRUISE AND ON FINAL APPROACH. EXPERIENCED UNCOMMANDED RUDDER MOVEMENT. RUDDER FLUTTER. DID NOT TURN OFF YAW DAMPENER. R AND R AHRS NR 2.

Part: COALESCER BAG — ODOR · airframe 28,855 hrs · 26,897 cycles

CREW REPORTED FUEL ODOR ON THE FLIGHT DECK (IN CRUSE) APU WAS NOT RUNNING. REMOVED AND REPLACED COALESCER SOCK IN AMM 21-51-13 RAN APU AND PERF OPS CHECKS OF PACKS DEFECTS ON ODORS NOTED.

Part: FIRE BOTTLE — LOW PRESSURE (CARGO BAY) · airframe 26,514 hrs · 24,647 cycles

RECEIVED CARGO BOTTLE LOW, CAUTION MESSAGE. R & R CARGO LEFT BOTTLE IAW 10-099. OPS CHECKED NORMAL.

Part: ROLLER — CHAFED (RT WING TE FLAP) · airframe 25,373 hrs · 23,409 cycles

RT OTBD FLAP INBD ROLLER IS WORN AND ROLLER GUIDE FITTING HAS MINOR CHAFING. R & R RT OTBD FLAP INBD ROLLER IAW SRM 51-41-01. FOUND CHAFE AT ROLLER GUIDE FITTING TO BE WITHIN ALLOWABLE LIMITS. REPAIRED FITTING IAW REO 601R-57-51-143 AND 601R-51-53-912.

Part: FLOORBEAM — CRACKED (FS 280.00) · airframe 25,373 hrs · 23,409 cycles

FLOOR STRUCTURE FS 280 IS CRACKED JUST OTBD OF LBL 9. C/W REO`S 601R-53-11-171, REV D AND 601R-53-11-2265 C/W NDT, NO DEFECTS NOTED.

Part: PANEL — GOUGED (LT WING) · airframe 25,373 hrs · 23,409 cycles

FUEL PANEL 540FB HAS GOUGE. REMOVED GOUGE IAW REO 601R-57-22-008. DID NOT EXCEED MAX RECORDED DEPTH.

Part: HINGE FITTING — GOUGED (RT AILERON) · airframe 25,373 hrs · 23,409 cycles

RT AILERON INBD HINGE FITTING HAS A GOUGE ON UPPER SURFACE. REMOVED GOUGE RT AILERON INBD HINGE FITTING IAW REO 601R-57-51-567. FOUND TO BE IN SERVICEABLE LIMITS. DID NOT EXCEED MAX RECORDED DEPTH.

Part: SILL — CORRODED (FS 319-349) · corrosion level 2 · airframe 25,373 hrs · 23,409 cycles

SERVICE DOOR LOWER SILL CAP FWD AND AFT EXTERNAL AND AFT INTERNAL HAS CORROSION AT FS 319.00 AND FS 349.00. REMOVED CORROSION AS REQUIRED IAW SRM 53-00-00. REPAIRED CROSSBEAM AT FS 349.00 IAW REO 601R-53-21-2245. APPLIED CPC AV 30 IAW SRM 51-21-11.

Part: HINGE FITTING — GOUGED (LT WING TE FLAP) · airframe 25,373 hrs · 23,409 cycles

LT INBD FLAP OTBD HINGE BOX ATTACH POINT ON WING HAS GOUGE. BLENDED GOUGE IAW REO 601R57-21-1589. FOUND TO BE IN SERVICEABLE LIMITS.

Part: BEARING — CRACKED (LT WING) · airframe 25,373 hrs · 23,409 cycles

LT WING HINGE PANEL 594JB OTBD ROLLER BEARING WORN AND HINGE PIN TAB CRACKED AND BENT. R & R OTBD LT WING HINGE PANEL ROLLER BEARING IAW RIL R26 NR2114. R & R HINGE, PN 601R10394 IAW SRM 51-42-06.

Part: HINGE — GOUGED (LT OTBD ELEVATOR) · airframe 25,373 hrs · 23,409 cycles

LEFT OTBD ELEVATOR HINGE ( HORIZONTAL STABILIZER SIDE) GOUGED. BLENDED GOUGE IAW REO 601R-55-11-402. FOUND TO BE IN SERVICEABLE LIMITS.

Part: SCUFF PLATE — CRACKED (FS 574) · airframe 25,373 hrs · 23,409 cycles

CARGO BAY DOOR SCUFF PLATE CRACKED AT SCREW HOLE. R & R SCUFF PLATE PN 601R-35022-35B IAW SRM 51-40-11 & 51-24-36, AMM 53-60-943-002.

Part: PANEL — CHAFED (LT WING TE FLAP) · airframe 25,373 hrs · 23,409 cycles

PANEL 584AB CHAFED ON L/E. REPAIRED IAW REO 601R-57-52-1833. FOUND TO BE WITHIN SERVICEABLE LIMITS.

Part: SKIN — DENTED (FS 579.00) · airframe 25,373 hrs · 23,409 cycles

CARGO DOOR CUTOUT LOWER FWD CORNER DENTED AT FS 579.00. BLENDED SHARP CORNER OF DENT SRM 51-12-00. AFTER REMOVAL OF SHARP EDGE DENT WAS NO LONGER DETECTED.

Part: LINK ASSY — CHAFED (THRUST REVERSER) · airframe 25,373 hrs · 23,409 cycles

RT THRUST REVERSER NR 1 LINK ARM CHAFED. BLENDED CHAFE IAW REO 601R-78-30-2940, FOUND TO BE WITHIN LIMITS.

Part: SUPPORT — CRACKED (PAX DOOR STEP) · airframe 25,373 hrs · 23,409 cycles

PAX DOOR LOWER STEP SUPPORT CRACKED. REPAIRED DAMAGED AREA ON PAX DOOR LOWER STEP SUPPORT IAW REO 601R-52-11-2028.

Part: FLOOR SUPPORT — CORRODED (BS 589-) · airframe 25,373 hrs · 23,409 cycles

FLOOR SUPPORT UNDER PANEL 281JLF HAS CORROSION AROUND NUTPLATES. REMOVED FLOOR SUPPORT CAP STRAP, DUPLICATED NEW STRIP OF LIKE MATERIAL & INSTALLED IAW SRM 51-00. 51-42-06, 51-42-211.

Part: FLOOR SUPPORT — CORRODED (BS 589) · airframe 25,373 hrs · 23,409 cycles

FLOOR SUPPORT UNDER PANEL 282GRF HAS CORROSION AROUND NUTPLATES. REMOVED FLOOR SUPPORT GAP STRIP, DUPLICATED NEW STRIP OF LIKE MATERIAL & INSTALLED IAW SRM 51-00, 51-42-06, 51-42-21.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 25,373 hrs · 23,409 cycles

LEFT MOST INBD FLAP L/E CHAFED OUT OF LIMITS. REMOVED UNSERVICEABLE LT MOST INBD FLAP LE SKIN AND REPLACED WITH NEW IAW SRM 51-42-13.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 25,373 hrs · 23,409 cycles

CARGO TRACK CORRODED. R & R CARGO TRACK IAW SRM 51-40-11, AMM 53-01-11.

Part: SKIN — CHAFED (WING) · airframe 25,373 hrs · 23,409 cycles

CHAFING DAMAGE FROM PANEL 193AB ENDS OF BOTH LT AND RT WING LOWER SKIN. BLENDED CHAFED DAMAGE AREA IAW REO 601R-57-21-880, REV C.

Part: SILL — CRACKED (FS 589) · airframe 25,373 hrs · 23,409 cycles

FLOOR SILL INBD CARGO DOOR CRACKED AT FS 589.00. REPAIRED IAW REO 601R-53-61-433, REV B.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 25,373 hrs · 23,409 cycles

FLOOR SUPPORT UNDER PANEL 281JLF HAS CORROSION AROUND NUTPLATES. REMOVED FLOOR SUPPPORT CAP STRIP, DUPLICATED NEW STRIP OF LIKE MATERIAL AND INSTALLED IAW SRM 51-00, 51-42-06, 51-42-21.

Part: SILL — CORRODED (FS 589.00) · corrosion level 2 · airframe 25,373 hrs · 23,409 cycles

CARGO DOOR SILL RETAINER FUSELAGE SIDE PITTED. REMOVED UNSERVICEABLE CARGO LOWER SILL COAMING AND REPLACED WITH NEW SERVICEABLE COAMING IAW SRM 51-41-02 AND 51-40-11.

Part: SKIN — CHAFED (LT WING) · airframe 25,373 hrs · 23,409 cycles

FUEL PANEL CUTOUT 550HB IS CHAFED ON INBD AND OTBD EDGES. BLENDED DAMAGED AREA ON FUEL TANK CUTOUT, WITHIN LIMITS IAW REO 601R-57-21-030. NDT FOUND NO DEFECTS, SHOT PEENED AREA IAW SRM 51-24-11.

Part: STRUCTURE — CHAFED (LT WING TE FLAP) · airframe 25,373 hrs · 23,409 cycles

CHAFE AT LT OTBD FLAP, NEXT TO ROLLER. BLENDED CHAFE AT LT OTBD FLAP NEXT TO ROLLER. REMOVED 0.002 OF MATERIAL, AMOUNT ALLOWED 0.020. REMAINING AMOUNT OF MATERIAL IS WITHIN SERVICEABLE LIMITS IAW REO 601R-57-53-039.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,373 hrs · 23,409 cycles

CORROSION ON RT SEAT TRACK. R & R SEAT TRACK IAW SRM 51-40-11, AMM 53-01-11,

Part: FLOORBEAM — CRACKED (FS 280.00) · airframe 25,373 hrs · 23,409 cycles

FS 280 CLIPS CRACKED INBD AND OTBD SIDE OF RBL9 FLOORBEAM. R & R RBL9 INBD & OTBD CLIPS WITH NEW SERVICEABLE CLIPS IAW SRM 51-42-21 AND REO 601R-53-11-71, REV D.

Part: SKIN — CHAFED (RT WING AILERON) · airframe 25,373 hrs · 23,409 cycles

UPPER L/E SURFACE OF RT AILERON IS CHAFED. BLENDED CHAFE ON UPPER L/E RT AILERON IAW REO 601R-57-60-013.

Part: SEAT TRACK — CORRODED (FS 364.00) · corrosion level 2 · airframe 25,373 hrs · 23,409 cycles

FIRST SECTION OF SEAT TRACK HEAVILY CORRODED. R & R SEAT TRACK IAW SRM 51-40-11, AMM 53-01-11.

Part: STRUCTURE — CHAFED (RT WING AILERON) · airframe 25,373 hrs · 23,409 cycles

RT WING AILERON HAS MINOR CHAFING TOP LEADING EDGE. BLENDED CHAFE ON RT WING AILERON L/E IAW REO 601R-57-60-013.

Part: STRUCTURE — CHAFED (RT WING AILERON) · airframe 25,373 hrs · 23,409 cycles

RT AILERON HAS CHAFING ON L/E INBD OF PCU`S. BLENDED RT LOWER L/E AILERON IAW REO 601R-57-60-020.

Part: SKIN — ERODED (RT NOSE COWL) · airframe 25,373 hrs · 23,409 cycles

RT ENGINE NOSE COWL HAS EROSION ON L/E SKIN. REMOVED LIGHT EROSION FROM L/E LIP SKIN AND POLISHED WITH SCOTCHBRITE IAW REO 601R-71-61-2532. MON THICKNESS PRIOR TO BLENDING 0.050. MIN THICKNESS AFTER BLENDING 0.048. WITHIN LIMITS IAW REO 601R-71-61-2532.

Part: STRUCTURE — CHAFED (LT AILERON) · airframe 25,373 hrs · 23,409 cycles

LT AILERON LOWER L/E CHAFED. REMOVED CHAFING IAW REO 601R-57-60-020.

Part: LUG — CHAFED (LT MLG DOOR) · airframe 25,373 hrs · 23,409 cycles

LEFT MLG DOOR LUG CHAFED. REMOVED CHAFING IAW REO 601R-52-82-143.

Part: DOOR — CHAFED (LT MLG) · airframe 25,373 hrs · 23,409 cycles

LT MLG DOOR CHAFED IN 2 PLACES, BOTTOM L/E. REMOVED CHAFING IAW REO 601R-52-82-034.

Part: ROD — CHAFED (RT MLG DOOR) · airframe 25,373 hrs · 23,409 cycles

RT MLG DOOR ROD LUG CHAFED. C/W REO 601R52-82-143. MEASURED CHAFING AFTER BLENDING IAW REO STEP 1, ORIG MATERIAL 0.329, IN LIMITS IAW REO. C/W NDT, NO DEFECTS NOTED. RETURNED FINISH TO A023 IAW REO 601R-52-82-143.

Part: SKIN — CHAFED (LT AILERON) · airframe 25,373 hrs · 23,409 cycles

LEFT AILERON UPPER SKIN IS CHAFED ENTIRE LENGTH OF AILERON. REMOVED CHAFING IAW REO 601R-57-60-013.

Part: PANEL — CHAFED (LT AILERON) · airframe 25,373 hrs · 23,409 cycles

PANEL 599BB CHAFED. BLENDED PANEL 599BB DAMAGED AREA, FOUND REMAINING MATERIAL TO BE WITHIN SERVICEABLE LIMITS IAW REO 601R-57-60-020.

Part: STRUCTURE — CHAFED (RT MLG DOOR) · airframe 25,373 hrs · 23,409 cycles

RT MLG DOOR CHAFED ON FWD AND AFT EDGES. C/W REO`S 601R-52-82-034 & 601R-52-82-102. BLENDED, ALODINED, PRIMED & TOP COATED AFT LOCATION CHAFING.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 25,373 hrs · 23,409 cycles

LT INBD FLAP LOWER SKIN HAS DENT TOWARDS T/E AFT OF OTBD MLG TIRE. DENT ON LT INBD FLAP LOWER SKIN FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGED AREA IAW SRM 57-52-00, REPAIR NR 3.

Part: GUIDE — CHAFED (LT WING TE FLAP) · airframe 25,373 hrs · 23,409 cycles

LT OTBD ROLLER GUIDE CHAFED. BLENDED LT OTBD FLAP ROLLER GUIDE, REMAINING MATERIAL IS WITHIN SERVICEABLE LIMITS IAW REO 601R57-51-143, TOTAL AMOUNT REMOVED 0.008, MAX ALLOWED 0.005.

Part: LANDING GEAR — MALFUNCTIONED · airframe 25,176 hrs · 23,206 cycles

GEAR WAS SELECTED DOWN AT 150 KTS, FLAPS AT 30. A BANGING NOISE WAS HEARD COMING FROM THE NOSE AREA. IT TOOK APPROX 10-15 SECS BEFORE NOSE GEAR INDICATED GREEN WHICH OCCURRED AFTER THE MAIN GEAR SHOWED GREEN. NO GEAR UNSAFE INDICATION. OPEN

Part: SKIN — DAMAGED (755) · airframe 21,092 hrs · 18,859 cycles

FUSELAGE SKIN DENTED AND CRACK ON RT SIDE JUST FWD OF VERTICAL STABILIZER 67.5. REPAIRED DAMAGE TO FUSELAGE SKIN AND OTHER DAMAGE AT RT SIDE AT 67.5 IAW REO 601R-53-71-110, O SPLICED SECTION OF UPPER SKIN, SPLICED SECTIO OF AFT WEB STIFFENER. REPLACED 3 EA STRINGERS.

Part: SKIN — DAMAGED (BS 736 S25L-26R) · airframe 21,092 hrs · 18,859 cycles

ACFT SKIN WAS SCRATCHED AND DENTED AT FS 736, STR 26L AND STR 25R, DAMAGE IS ON BELLY, REF LOGBOOK PG 180013, BLOCK 2. COLD WORKED DENTS AND BLENDED MINOR SCRATCHES AND INSTALLED SERVICEABLE STR26L, IAW REO 601R-53-61-355.

Part: SKIN — DAMAGED (BS 755) · airframe 21,092 hrs · 18,859 cycles

REMOVED DAMAGED RT LOWER SKIN BETWEEN FS 755.0 AND 67.5 (VERTICAL STABILIZER REAR SPAR). R & R WITH SERVICEABLE SKIN.

Part: ANGLE — DAMAGED (BS 67.5) · airframe 21,092 hrs · 18,859 cycles

REMOVED DAMAGED RT CTR SECTION OF CORNER CAP ANGLE (VERTICAL STABILIZER REAR SPAR). REMOVED DAMAGED RT CTR SECTION OF CORNER CAP ANGLE AND INSTALLED SERVICEABLE CORNER CAP ANGLE.

Part: FINGER DOUBLER — DAMAGED (FUSELAGE) · airframe 21,092 hrs · 18,859 cycles

REMOVED DAMAGED LOWER RT OTBD FINGER DOUBLER FROM FS 67.5 FROM STR 13R TO STR 26R IAW SRM 51-42-06. INSTALLED SERVICEABLE RT LWR DOUBLER AT 67.5 FROM STR 13R TO STR 26R IAW SRM 51-42-06.

Part: STRINGER — DAMAGED (BS 755) · airframe 21,092 hrs · 18,859 cycles

MWC 51589-3000-0004- AIRCRAFT DAMAGE FOUND ON STRINGERS JUST FWD OF AFT BULKHEAD. FWD STRINGER 12R,13R, & 14R (REF LOGBOOK 180012, BLOCK) FROM FS 755 TO VERTICAL STABILIZER REAR SPAR. R & R STR 12R, & STR 14R IAW SRM 51-42-06.

Part: BRACKET — CRACKED (BS 528) · airframe 20,983 hrs · 18,743 cycles

BRACKET ON TOP OF LT MLG WW IS CRACKED. R & R BRACKET IAW REO 601R53-42-007.

Part: SEAT TRACK — CORRODED (BS 364) · corrosion level 2 · airframe 20,983 hrs · 18,743 cycles

NR 1 SEAT RAIL RT INBD CORRODED. REMOVED UNSERVICEABLE NR 1 RT INBD SEAT RAIL AND INSTALLED SERVICEABLE NR 1 RT INBD SEAT RAIL.

Part: RETAINER — GOUGED (RT PYLON) · airframe 20,983 hrs · 18,743 cycles

RT PYLON PANEL 422AB SUPPORT ANGLE IS GOUGED. REMOVED DAMAGED SEAL RETAINER AND INSTALLED SERVICEBLE RETAINER.

Part: HINGE FITTING — GOUGED (RT NACELLE) · airframe 20,983 hrs · 18,743 cycles

RT ENGINE UPR TRANS COWL INNER INBD HINGE FITTING IS GOUGED. REPAIRED GOUGE IAW REO 601R-78-33-3923.

Part: HINGE FITTING — GOUGED (RT NACELLE) · airframe 20,983 hrs · 18,743 cycles

RT ENGINE LWR TRANS COWL INNER INBD CTR HINGE FITTING IS GOUGED. REPAIRED GOUGE IAW REO NR 601R-78-33-3922.

Part: STIFFENER — CRACKED (BS 559) · airframe 20,983 hrs · 18,743 cycles

FOUND (VISUAL) RBL 18 STIFFENER ON FS 559 BULKHEAD CRACKED AT LOWEST OTBD RIVET. COMPLIED WITH REPAIR OF RBL 18 STIFFENER ON FS 559 BULKHEAD BY INCORPORATION OF REO`S 601R-53-41-260, AND 601R-53-41-609.

Part: WEB — CRACKED (BS 718) · airframe 20,983 hrs · 18,743 cycles

HYD SYS NR 1 FWD ACCUMULATOR MOUNT WEB CRACKED UNDER MOUNT INSTALLED NEW WEB PN 600-75221-109.

Part: INTERCOSTAL — CRACKED (APU DOOR) · airframe 20,983 hrs · 18,743 cycles

INTERCOASTAL FUSELAGE IS CRACKED ON FWD END (AT APU DOOR ACTUATOR). REMOVED AND REPLACED INTERCOSTAL.

Part: DUCT — CRACKED (APU INTAKE) · airframe 20,983 hrs · 18,743 cycles

APU UPPER INTAKE DUCT CRACKED, REMOVED AND REPLACED.

Part: STRUCTURE — DAMAGED (RT PYLON) · airframe 20,983 hrs · 18,743 cycles

RT PYLON PANEL 422DB DIVIDER ARE BOTH CRACKED. REMOVED DAMAGED RT PYLON PNL 422DB DIVIDERS AND INSTALLED 2 EA SERVICEABLE DIVIDERS IAW SRM 51-42-10, 51-42-10.

Part: SEAL — DAMAGED (LT FLT SPOILER) · airframe 20,983 hrs · 18,743 cycles

METAL SEAL UNDER LT FLIGHT SPOILER BETWEEN CENTER HINGES IS CRACKED. REMOVED DAMAGED SEAL AND INSTALLED SERVICEABLE SEAL.

Part: STRUCTURE — CRACKED (APU BAY) · airframe 20,983 hrs · 18,743 cycles

APU ENCLOSURE CRACKED ON AFT SIDE ON DOOR MATING SURFACE REPAIRED CRACKS IAW REO 601R-49-11-070.

Part: BRACKET — CORRODED (BS 344) · corrosion level 2 · airframe 20,983 hrs · 18,743 cycles

CORROSION ON PAX DOOR CUT-OUT SILL, AFT HANDRAIL CLEAT AND BRACKET. R & R PAX DOOR CUT-OUT AFT HANDRAIL CLEAT BRACKET WITH SERVICEABLE PN 601R31527-217 BRACKET AND PN 601R31527-137 CLEAT, IAW SRM 51-42-06 AND 51-42-13.

Part: BRACKET — CORRODED (PAX DOOR) · corrosion level 2 · airframe 20,983 hrs · 18,743 cycles

CORROSION ON PAX DOOR C/O SILL, AFT HANDRAIL CLEAT AND BRACKET. REMOVED AND REPLACED PAX DOOR C/O AFT HANDRAIL CLEAT AND BRACKET WITH SERVICEABLE P/N 601R31527-217, PRACKET & PN 601R31527-137 CLEAT, IAW SRM 51-42-06 & 51-42-13.

Part: STIFFENER — CRACKED (APU DOOR) · airframe 20,983 hrs · 18,743 cycles

APU ENCLOSURE DOOR AFT STIFFENERS CRACKED ON UPPER END REPAIRED CRACKS IAW REO 601R-49-11-070.

Part: SKIN — CRACKED (PAX DOOR) · airframe 20,983 hrs · 18,743 cycles

PAX DOOR FWD SIDE SKIN CRACKED AT HANDRAIL. REMOVED DAMAGED AREA AND REPLACED WITH 2 EACH REPAIR ANGLES AND EXTERNAL DOUBLER IAW REO 601R-52-11-702.

Part: DOOR FRAME — CRACKED (PAX DOOR) · airframe 20,983 hrs · 18,743 cycles

FRAME ANGLE BELOW PAX DOOR PANEL 832AR CRACKED. REMOVED CRACKED FRAME ANGLE AND INSTALLED NEW SERVICEABLE PN 601R-318094-2.

Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 20,983 hrs · 18,743 cycles

PAX DOOR VENT FLAP AFT ATTACH ANGLE APPEARS TO BE CRACKED. REMOVED CRACKED ATTACH ANGLE AND DUPLICATED IAW SRM 51-24-24.

Part: CHANNEL — CRACKED (DOOR CUTOUT) · airframe 20,983 hrs · 18,743 cycles

U-CHANNEL CRACKED ON FWD SIDE OF CARGO DOOR CUTOUT (LOWER DOOR TRACK ATTACHMENT) REMOVED DAMAGED BRACKET AND DUPLICATED AND INSTALLED NEW BRACKET.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 20,983 hrs · 18,743 cycles

LT OTBD FLAP OTBD HINGE ARM HAS CRACKED FAIRING ATTACH ANGLE ON INBD SIDE. R & R ANGLE AT LT OTBD FLAP OTBD HINGE INBD SIDE IAW SRM 57-54-00, 51-40-00, 51-40-11, 51-42-13.

Part: O-RING — CUT (EDP) · airframe 20,637 hrs · 18,415 cycles

RT ENG OIL PSI WARNING MSG DISPLAYED IN FLIGHT C/W QRH. REDUCED POWER TO IDLE FOR REMAINDER OF FLIGHT. AT IDLE OIL PSI INDICATED 36 PSI AND OIL TEMP AT 80 DEG. LANDED ACFT BELOW 47,000 LBS. FOUND O-RING AT EDP CARBON SEAL CUT REPLACED IAW AMM 72-60-00. PERFORMED OIL CONSUMPTION RUN IAW AMM 71-00-00. OPS AND LEAK CK GOOD. (K)

Part: A/C PACK — ODOR (LEFT) · airframe 19,840 hrs · 17,635 cycles

LEFT AC PACK HAS FUEL ODOR AT HIGHER DUCT TAPS. RAN BOTH PACK OFF ENGINE BLEED AIR NO FUEL SMELL. (K)

Part: CONNECTOR — DAMAGED (NR 1 TEMP) · airframe 19,786 hrs · 17,582 cycles

ON CLIMBOUT, HAD A MASTER CAUTION ON IDG 1. REMOVED AND REPLACED NR 1 ENG IDG TEMP BULB AND TEMP BULB CONNECTOR IAW 24-13-05. OPS CHECK GOOD. (K)

Part: LIGHT — DAMAGED (COCKPIT) · airframe 19,180 hrs · 17,002 cycles

AT 11,000 FT SMOKE IN COCKPIT AFTER ADJUSTING F/O FLOODLIGHT, FOLLOWED 1AC AND QRH SMOKE SUBSIDED, DECLARED EMERGENCY, LANDED, FOUND CBP4C1 POPPED. INSPECTED AND FOUND F/O FLOODLIGHT DAMAGED, INSPECTED AREA, NO FURTHER DAMAGE TO SURROUNDING AREA REF 198190/2 FOR MEL. REMOVED AND REPLACED F/O FLOODLIGHT AND PERFORMED OPS CHECK IAW AMM 33-11-00. CHECKS GOOD REMOVED FROM PLACARD AND MEL. (K)

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 18,588 hrs · 16,450 cycles

LOG 186985/3 - FLAPS FAIL INFLT DURING EXTENSION AT ZERO DEGREES PERFORMED FLAP RESET IAW SUPP 98-018B STEPS 1.3 AND 1.4, FLAP RESET. COMPLIED WITH FIM 27-50-00 AND FOUND THE INPUT TORQUE OUT OF LIMITS ON LT FLAP DRIVE SYS. FOUND LT INBD FLAP INBD ACTUATOR THE CAUSE OF HIGH TORQUE. R&R LT INBD FLAP INBD ACTUATOR IAW AMM 27-53-01. OPS AND RIG CHECK GOOD. LT FLAP DRIVE SYS INPUT TORQUE WITHIN LIMITS AT THIS TIME. COMPLIED WITH AWAC SUPP 98-018B AND 07-008B.

Part: TARGET — LOOSE (MLG) · airframe 16,788 hrs · 14,739 cycles

ON DEPARTURE, AFTER LANDING GEAR RETRACTION RECEIVED GEAR DISAGREE MASTER WARNING RT MAIN GEAR C/W QRH DIVERTED IAD GEAR INDICATED 3 GREEN. FOUND RT MLG UPLOCK TARGET LOOSE. RETORQUED AND PERFORMED GEAR SWINGS PER AMM 32-30-00. REMOVED FROM MEL.

Part: DIAPHRAGM — MISSING (RUDDER) · airframe 16,561 hrs · 14,522 cycles

RUDDER UPPER CLOSURE RIB IS MISSING DIAPHRAGM CLOTH. REPAIRED IAW CRJ 200 REO 601R-55-41-037. (M)

Part: FAIRING — DAMAGED (TE FLAP) · airframe 16,561 hrs · 14,522 cycles

ABRASION FOUND ON LEFT FLAP STUB FAIRING EXTERNAL SURFACE. (M) REPLACED IAW SRM 51-42-06. (K)

Part: BULKHEAD — CRACKED (BS 202) · airframe 16,561 hrs · 14,522 cycles

FORWARD PRESSURE BULKHEAD AT FS 202.75 LBL 23.71, WL 69 IS CRACKED. REPAIRED IAW REO 601R-53-11-563. (M)

Part: FAIRING — DAMAGED (TE FLAP)

ABRASION FOUND ON RT FLAP STUB FAIRING EXTERNAL SURFACE. (M) REPLACED IAW SRM 51-42-06, 51-41-02, 51-42-11. (K)

Part: HINGE — CRACKED (DOOR STEP) · airframe 16,561 hrs · 14,522 cycles

PAX DOOR FOLDING STEP UPPER HINGE, REF P/N 601R31980-41, AND LOWER HINGE , REF P/N 601R31980-63 FOUND CRACKED. (M)

Part: ANGLE — CRACKED (BS 621) · airframe 16,561 hrs · 14,523 cycles

TWO ANGLES CRACKED ON THE REAR PRESSURE BULKHEAD AT RBL AND LBL 46 FS 621 AND WL 93.50. TWO ANGLES ON THE REAR PRESSURE BULKHEAD REPLACED IAW REO 601R-53-61-100 REV A. (M)

Part: SILL — CORRODED (BS 310-349) · corrosion level 1 · airframe 16,561 hrs · 14,522 cycles

SERVICE DOOR LOWER SILL PLATE CORRODED. BLENDED IAW SRM 51-21-06. (K)

Part: DIAPHRAGM — MISSING (RUDDER) · airframe 16,561 hrs · 14,522 cycles

RUDDER LOWER CLOSURE RIB IS MISSING CLOTH DIAPHRAGM. REPAIRED IAW CRJ 200 REO 601R-55-41-018 REV A. (M)

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 16,561 hrs · 14,522 cycles

OUTBOARD CLIP AT FS 484 RBL 36 FOUND CRACKED. REPLACED IAW CRJ 200 REO 601R-53-41-059 REV A. (M)

Part: STRIP — WORN (NOSE COWL) · airframe 16,561 hrs · 14,522 cycles

RIGHT NOSE COWL UPPER DOOR AFT STRIP FOUND WORN. REPAIRED IAW CRJ 200 CMM 71-14-01-300-815- A01. (M)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,561 hrs · 14,522 cycles

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

Part: STEP — CRACKED (PAX DOOR) · airframe 16,561 hrs · 14,522 cycles

PAX DOOR STAIR AFT WEB CRACK ON 1ST AND 2ND STEP CORNER AREA. REPAIRED IAW REO 601R-52-11-702 REV A. (K)

Part: HINGE — CRACKED (FOLDING STEP) · airframe 16,561 hrs · 14,522 cycles

PAX DOOR FOLDING STEP UPPER HINGE, REF P/N 601R31980-41, AND LOWER HINGE, REF P/N 601R31980-63, FOUND CRACKED. REPLACED PAX DOOR FOLDING STEP UPPER HINGE IAW SRM 51-42-02 AND REPLACED LOWER HINGE IAW SRM 51-41-02. (M)

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 16,561 hrs · 14,522 cycles

ON PAX DOOR, STIFFENER ANGLE FOUND CRACK. STIFFENER ON PAX DOOR FS 349. REPLACED IAW SRM 51-42-06. (M)

Part: FLOORBEAM — CRACKED (BS280) · airframe 16,561 hrs · 14,522 cycles

CROSSBEAM AT FS 280 RBL 9.0, WL 72 IS CRACKED IN RADIUS. (M) REPAIRED IAW REO 601R-53-11-171, REV B. (K)

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 16,561 hrs · 14,522 cycles

INTERCOSTAL AT FS 484 INBOARD CLIP AT RBL 27 IS CRACKED. REPLACED. (M)

Part: BULKHEAD — CRACKED (BS 621)

PRESSURE BULKHEAD WEB AT FS 621, LINTEL AREA, IS CRACKED. REPAIRED IAW CRJ 200 REO 601R-53-61-1230 REV D. (M)

Part: HANDLE — SEIZED (ESCAPE HATCH) · airframe 16,660 hrs · 14,621 cycles

FAILURE OF FUNCTIONAL TEST OF CREW ESCAPE HATCH, OUTER HANDLE SEIZED DUE TO CORROSION, DURING C-CHECK. CREW ESCAPE HATCH OUTER HANDLE REPLACED. (M)

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (MLG)

GROUND LIFT DUMP UNSAFE CAUTION MESSAGE IN FLIGHT. QRH PROCEDURE CLEARED MESSAGE. COMPLIED WITH OPS CHECK OF SPOILER FLIGHT SYSTEM. IAW SYS IAW AMM 27-60-00 PARA 11. THIS MESSAGE IS CAUSED BY ANIT-SKID PROBLEM. REMOVED AND REPLACED IAW 32-44-06. OPS CHECK GOOD AT THIS TIME/ REF LP 198609/4 FOR ANTI-SKID WRITE UP. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT IAW 32-44-06. OPS CHECK GOOD. (K)

Part: THERMAL SWITCH — INOPERATIVE (LT WING) · airframe 16,079 hrs · 14,062 cycles

WING OVERHEAT WARNING MESSAGE ON CLIMBOUT SYNOPTIC PAGE SHOWS LT WING. COMPLIED WITH QRH, MESSAGE CLEARED. IN OFF, AND APPROXIMATELY 1 MINUTE LATER, REAPPEARED IN STANDBY. REMOVED AND REPLACED LT WING STANDBY THERMAL SWITCH IAW AMM 30, OPS CHECK GOOD. (K)

Part: WARNING MESSAGE — ILLUMINATED (WING OVERHEAT) · airframe 16,065 hrs · 14,045 cycles

WING OVERHEAT WARNING MESSAGE ON CLIMBOUT, SYNOPTIC PAGE INDICATES LT WING. CORRECTIVE ACTION IN PROGRESS. (K)

Part: FIRE BOTTLE — LOW (CARGO BAY)

CARGO BOTTLE LOW MESSAGE. COMPLIED WITH QRH, MESSAGE CLEARED DESCENT. FIRE DEPARTMENT INSPECTION FOUND NO EVIDENCE OF HEAT. PLACED ON MEL. REMOVED AND REPLACED LT FIRE BOTTLE, OPS CHECK GOOD IAW 26-20-00 REMOVED OFF MEL.

Part: UNKNOWN — WARNING LIGHT (WINDSHIELD HEAT) · airframe 14,372 hrs · 12,369 cycles

LT WINDSHIELD HEAT MESSAGE ILLUMINATED IN FLIGHT. COMPLIED WITH QRH. [07-31-07] COMPLIED WITH CONNECTION OF SPARE TEMP SENSORS IAW AMM 30-41-06. OPS CHECK GOOD. (K)

Part: SERVICE DOOR — MALFUNCTIONED · airframe 14,193 hrs · 12,188 cycles

SERVICE DOOR WILL NOT OPEN. CYCLED DOOR, OPENED NORMAL. (K)

Part: CONNECTOR — LOOSE (SPOILER PCU)

UNCOMMANDED ROLL FLAPS 45 AIRSPEED MANEUVERING OR GREATER, R-TURN 10-15 DEGREES BANK ANGLE AIRCRAFT CONTINUES TO ROLL INTO TURN. INSPECTED RIGHT SPOILER OUTBOARD PCU AND FOUND CANNON PLUG LOOSE. RESECURED AND PERFORMED OPS CHECK OF RT SPOILERON IAW AMM 27-60-00. OPS CHECK GOOD. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

CRACKED RIGHT WINDSHIELD, HAPPENED DURING TAXI OUT. REMOVED AND REPLACED WINDSHIELD, OPS CHECK GOOD IAW AMM 56-11-01. (M)

Part: CONNECTOR — BROKEN (CABIN)

FOUND FLOOR TRACK LIGHTING CONNECTOR AT LAV BROKE. REMOVED AND REPLACED CONNECTOR ON FLOOR TRACK LIGHTING AT LAV IAW CRJ WM 20-17-10. OPERATIONAL CHECK GOOD CRJ AMM 33-51-00-710-801. (M)

Part: CLIP — CRACKED (FUSELAGE) · airframe 11,564 hrs · 9,684 cycles

FS 280 CLIP AT LBL 9.0, OB, IS CRACKED NEAR RADIUS APPROX .60 INCH LONG. MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM. LT OB FS 280. (K)

Part: BEAM — CORRODED (FUSELAGE) · airframe 11,564 hrs · 9,684 cycles

J-ANGLE ON TRANSVERSE BEAM FS 280 BETWEEN LBL 9.0 AND RBL9.0 HAS AREAS OF CORROSION AT CAMLOCK RECEPTICAL. LARGEST AREA MEASURES APPROX 1.5 INCH L X 1.0 INCH W X .009 INCH D. MAINTENANCE REMOVED DAMAGE ANGLE AND INSTALLED NEW ANGLE IAW SRM. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 11,564 hrs · 9,684 cycles

FS 280 CLIP AT LBL 9.0, IB, IS CRACKED NEAR RADIUS APPROX .80 INCH LONG. MAINTENANCE REMOVED AND REPLACED CLIP AT IB LT FS 280 IAW SRM. (K)

Part: BEAM — CORRODED (FUSELAGE) · airframe 11,564 hrs · 9,684 cycles

TRANSVERSE BEAM AT FS 280 BETWEEN LBL 9.0 AND RBL 9.0 HAS SEVERAL AREAS OF CORROSION. LARGEST AREA MEASURES APPROX 3.5 INC X .80 INCH W .007 INCH D. MAINTENANCE REMOVED DAMAGE SECTION OF TRANSVERSE BEAM (J ANGLE) AND INSTALLED REPLACED ANGLE IAW EO. (K)

Part: CLIP — CRACKED (FUSELAGE) · airframe 11,564 hrs · 9,684 cycles

FS 280 CLIP AT RBL 9.0, IB, IS CRACKED NEAR RADIUS APPROX .90 INCH LONG. MAINTENANCE REMOVED AND REPLACED CLIP IAW SRM. RT IB FS 280 FRAME. (K)

Part: CLIP — CRACKED · airframe 11,564 hrs · 9,684 cycles

FS 280 CLIP AT RBL 9.0, OB, IS CRACKED NEAR RADIUS APPROX .80 INCH LONG. MAINTENANCE REMOVED AND REPLACED ANGLE IAW SRM. RT OB FS280. (K)

Part: DISPLAY — MALFUNCTIONED (COCKPIT)

CAPTAINS MFD FAILED INFLIGHT, UNABLE TO USE REVISIONARY FUNCTION F/O PFD ERRATIC AND STAB TRIM 1 AND 2 AND MACH TRIM DISENGAGES. INTERROGATED MDC, NO CURRENT FAULTS FOUND, RE-SET CAPTS MFD CB FOR FAILED CAPTS MFD, CND. FAULT PERFORMED NR 1 AND NR 2 ENGINE RUNS CYCLED 1 AND 2 GENERATOR MFD AND PFD FOR FAULTS. PERFORMED HFTCU FAULT ISOLATION TASK IAW 27-40-00 FOR STAB TRIM DISENGAGED. (M)

Part: SCREEN — DIRTY (CABIN)

DISPLAY COOL CAUTION MESSAGE INFLIGHT. MESSAGE WAS INTERMITTENT REGARDLESS OF FAN SELECTION. INSPECTED DISPLAY COOLING DUCTING, NO LEAKS NOTED. AIR FILTER GETTING DIRTY HOWEVER NOT CLOGGED. CLEANED AIR SCREEN BEHIND PFD2. ALL THREE FANS BLOW NORMALLY. NO FAULTS NOTED IAW AMM 21-24-00 AND 21-24-14 AND 21-24-19. (M)

Part: CONTROL SYSTEM — BINDING (AILERONS) · airframe 8,827 hrs · 7,363 cycles

FIRST OFFICER REPORTED RT AILERON BINDING ON APPROACH WITH AUTO PILOT SELECTED OFF. INSPECTED AILERON CONTROL SYSTEM IAW SL. FOUND NO EVIDENCE OF MOISTURE OR PULLEY BINDING. NO FAULTS IN MDC. PERFORMED OPS CHECK OF AUTOPILOT, OPS CHECK GOOD IAW 27-11-00.

Part: DUCT — SEPARATED (COCKPIT)

MESSAGE IN FLIGHT, QRH COMPLIED WITH. DISPLAY COOL MESSAGE INTERMITTENT IN FLIGHT. ALT POSITION WENT TO STANDBY POSITION THEN EXTINGUISHED THRU FL270 THEN WENT OFF (AIR RETURN). UPON INSPECTION FOUND DUCT ABOVE CAPTAINS RUDDER PEDAL OFF. RESECURED DUCT. OPS CHECK GOOD IAW AMM21-24-22.

Part: SILL — CRACKED (FUSELAGE)

FOUND FLOOR SILL PLATE AT CARGO DOOR ENTRANCE IS CRACKED. CUT OUT DAMAGED SECTION OF FLOOR SILL SECTION AND INSTALLED FABRICATED REPAIR SECTION OF FLOOR SILL AND INSTALLED FABRICATED SPLICE DOUBLER IAW BRAS EO 601R-53-5095. (M)

Part: SKIN — DENTED (HORIZONTAL STAB)

DENT IN LEFT HORIZONTAL STABILIZER BOTTOM SKIN APPROXIMATELY 74 INCHES FROM VISOR AND 9 INCHES FROM 4E. PERFORMED A MAJOR REPAIR IAW BRAS EO 601R-55-5102 BY DRILLING NR 30 HOLE IN DAMAGE AREA AND PULLING DENT TO ORIGINAL CONTOUR. PERFORMED EDDY CURRENT INSPECTION TO ENSURE NO CRACKS EXIST AND INSPECTED FOR OIL CANNING. FILLED HOLE WITH CR3214 RIVET. (M)

Part: BUSHING — LOOSE (RT MLG)

RIGHT MAIN LANDING GEAR AFT TRUNNION BUSHING IS MIGRATED .062 INCH. PERFORMED A MAJOR REPAIR TO MIGRATED RIGHT MLG AFT TRUNNION BUSHING BY REMOVING BUSHING AND INSTALLING 1ST OVERSIZE BUSHING P/N 601R-57-21-003-21 IAW BOMBARDIER REO 601R-57-21-003 REV B. (M)

Part: ANGLE — CRACKED (PAX DOOR STAIR)

PAX DOOR STAIR STRUCTURE AFT ANGLE, PN 601R31907-303, IS CRACKED .8 INCHES LONG AREA OF DOOR ASSIST CABLE PULLEY BRACKET LOCATED IN RADIUS OF ANGLE. REMOVED CRACKED ANGLE AND INSTALLED A NEW ANGLE PN 601R311719 IAW REO 601R53-41-059.

Part: AIRSTAIR — CRACKED (FUSELAGE)

PASSENGER DOOR STAIR STRUCTURE AFT ANGLE IS CRACKED .80 INCH LONG IN AREA OF DOOR ASSIST CABLE PULLEY BRACKET LOCATED IN RADIUS OF ANGLE. CUT AWAY DAMAGED SECTION OF DRAG ANGLE, FABRICATED REPLACEMENT DRAG ANGLE FROM 5773 EXTRUSION AND SPLICE ANGLES FROM $6144-14 ANGLE. INSTALLED ANGLES IAW BRAS EO 601R-52-5101A AND CRJ SRM 51-23-00. (M)

Part: ANGLE — CRACKED (AIRSTAIR)

PASSENGER DOOR STAIR STRUCTURE AFT ANGLE, P/N 601R31907-303 IS CRACKED .8 INCH LONG AREA OF DOOR ASSIST CABLE PULLEY BRACKET LOCATED IN RADIUS OF ANGLE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

FOUND RIGHT SIDE FS 621/FS 625 OBLIQUE ANGLE AT STRINGER 14R IS CRACKED IN RADIUS APPROXIMATELY 1 INCH. REPLACED CRACKED ANGLE WITH NE ANGLE P/N 601-35012-52 IAW CRJ SRM 51-42-06. (M)

Part: ACCESS DOOR — CORRODED (RT WING)

RIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUT OT AT WS 54.897 HAS FRETTING DAMAGE IN TWO AREAS, INBOARD AND FORWARD .004 IN CHES DEEP AT WORST AREA. REMOVED FRETTING CORROSION ON LOWER WING PLANK FUEL ACCESS DOOR IN THREE PLACES (.004 DEEP) WS 54.897 PANEL 640BB IAW BOMBARDIER REO 601R-57-21-030 REV C. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FOUND FLOOR SUPPORT ANGLE BRACKET IS CRACKED AT FS 484, LEFT SIDE, LBL 36. REMOVED CRACKED ATTACHMENT FLANGE AND FABRICATED NEW REPAIR ANGLE, P/N 1 FORM 6144-14 AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059 AND BRAS EO 601R-53-0030. (M)

Part: ATTACH ANGLE — CRACKED (FUSELAGE)

ATTACHMENT ANGLES AT FS 621 CRACKED AT LEFT/RIGHT SIDES. PERFORMED A MAJOR REPAIR TO CRACKED UNDER FLOOR SUPPORT ANGLE AT FS 621 LEFT SIDE AND RT SIDE BY REMOVING CRACKED SECTION OF ANGLE AND INSTALLING REPAIR IAW BOMBARDIER REO 601R-53-61-117 REV B. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FOUND FLOOR SUPPORT ANGLE CRACKED AT FS 484 RBL 27. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

FLOOR SUPPORT ANGLE AT FS 484 RBL 36 IS CRACKED. REMOVED CRACKED ATTACHMENT FLANGE, FABRICATED NEW REPAIR ANGLE,P/N 2 FROM 6144-14 AND INSTALLED IAW BOMBARDIER REO 601R-53-41-059 AND BRAS EO 601R-53-0030. (M)

Part: ANGLE — CRACKED (LT FUSELAGE)

FOUND LEFT SIDE FS 621/FS 625, OBLIQUE ANGLE AT STRINGER 14L IS CRACKED IN RADIUS APPROXIMATELY 1.1 INCH LONG, 1.1 INCHES. REPLACED CRACKED ANGLE WITH NEW ANGLE, P/N 601-35012-51, IAW CRJ SRM 51-42-06. (M)

Part: ACM — FAILED (RIGHT) · airframe 5,898 hrs · 4,839 cycles

ON TAXI, CABIN BEGAN TO FILL WITH SMOKE. PLACED RT PACK ON MEL. RT PACK MAKING LOUD GRINDING NOISE AND EXCESSIVE VIBRATION. RAN RIGHT ENGINE, CHECKED NR 2 BLEED AND APU BLEED ON NR 1 PACK. NO SMOKE NOTED. REMOVED AND REPLACED AIR CYCLE MACHINE IAW AMM. OPS CHECK GOOD. (M)

Part: ACTUATOR — MALFUNCTIONED (YAW DAMPER)

YAW DAMPER NR 2 WILL NOT STAY ENGAGED WHEN MOVING AIRCRAFT. YAW DAMP INOPERATIVE STATUS MESSAGE. REMOVED AND REPLACED NR 2 YAW DAMPER ACTUATOR. CHECKS OK. (M)

Part: ODOR — DETECTED (CABIN)

APU AUTO SHUTDOWN IN FLIGHT, CREW RESTARTED INFLIGHT, STRONG FUEL SMELL IN CABIN AFTER APU BLEED AIR SELECTED ON TO FEED PACKS, FUEL ON TAIL OF AIRCRAFT ON GROUND. MAINTENANCE INSPECTED APU WITH APU RUNNING, NO FUEL LEAKS, CHECKED APU OIL LEVEL OK. OPERATED PACKS NO SMELL NOTED. (M)