N444ZW
Registered owner: UMB BANK NA TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AIR WISCONSIN AIRLINES CORPORATION | Operator | 2021-09-17 – 2021-09-17 | Operator named in NTSB report |
| AIR WISCONSIN AIRLINES LLC (A6WA) | Operator | 2021-09-17 – 2021-09-17 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
REQUEST INSPECTION FOR SHORTED GROUND POWER RECEPTACLE. AC GROUND POWER AIRCRAFT REMOVED FROM SERVICE. INSPECTED AND FND A/C RECEPT AND SHIELD MELTED, RECEPT SUPPORT MEMBER & INTERCOSTAL HAS HEAT DAMAGE AND MELTED AREAS. FWD PRESS BULHEAD HAS APPROX 2"X 1.5" HOLE IN IT WITH SURROUNDING AREA METAL DISCOLORED, WARPED AND CRACKING. BLKHD VERT STIFFNER AND NLG BAY WEB HAVE SPARKING DAMAGE SIMILAR TO LIGHTNING STRIKE. RIVETS AT FS199 FOR RECEPT INTERCOSTAL HAVE BEGUN TO MELT, BUT ARE NOT NOT LOOSE. REF 370607-3 FOR OPS CK OF AC PWR GEN SYSTEMS REF 370607-1FOR ORIG DISCREPANCY
AFTER DEPARTURE AND SELECTING LANDING GEAR LEVER TO UP POSITION, RECEIVED NOSE DOOR OPEN WARNING AND NOSE STEERING INOP CAUTION, WOW INPUT CAUTION AND WOW OUTPUT STATUS. C/W QRH. NLG INDICATING DOWN AND LOCK AND LT AND RT MLG INDICATED UP AND LOCKED. AIRCRAFT REMOVED FROM SERVICE. SVCD NLG STRUT REF AMM 12-12-32 PERFORMED NLG SWING, SWING GOOD AT THIS TIME EXT CHECK AFTER PERFORMED AFT 24 HRS AT NEXT A CHECK PER AMM SUP 16-250A.
6171 - SHORTLY AFTER TAKEOFF HYD 3 LOW PRESSURE CAUTION MESSAGE. C/W QRH MESSAGE CLEARED. AIRCRAFT REMOVED FROM SERVICE. PER OPS CK SYS 3A AND 3B PER AMM 29-12-03 OPS CK GOOD AT THIS TIME
CORROSION ON BRACKET AT WS 48.30 AT LH TE WING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BRACKET AT WS 48.30 AT LH TE WING REF. CRJ-200 SRM 51-42-06 AND 51-42-20 REV. 39. RESTORED PROTECTIVE FINISH. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 004235, CARD NO. 50102, TT: 41,109 TC: 39,987.
POSSIBLE CORROSION ON ENTRY DOOR SILL AT FS310.00 TO FS349.00 LBL 40 TO 44. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FWD & AFT BRACKETS WITH P/N 601R31527-217 & FABRICATED NEW CLEAT WITH P/N 601R31527-176, ON SURROUND STRUCTURE AT PAX DOOR I.A.W. CRJ-200 SRM 51-42-06 REV. 39. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 004309, CARD NO. 20031, TT: 47,227:03 TC: 44,966.
CABIN RH FLOOR SILL SUPPORT PN 601R31133-102 AND PLATE PN 601R31133-101 AT FS559.00 + 85 TO FS559.00 + 116 AND RBL42 TO RBL44 HAS EXFOLIATION CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED CABIN RH FLOOR SILL SUPPORT PN 601R31133-102 AND PLATE PN 601R31133-101 AT FS559.00 + 85 TO FS559.00 + 116 AND RBL42 TO RBL44. ALL WORK WITHIN LIMITS WAS PERFORMED IAW AIR WISCONSIN CRJ200 SRM 53-00-00 REV 39, CRJ200 SRM 51-21-06 REV 39, CRJ200 SRM 53-51-43 REV 39, CRJ200 SRM 51-42-06 REV 39, CRJ200 SRM 51-11-00 REV 39, CRJ200 SRM 51-40-11 REV 39, CRJ200 SRM 51-42-15 REV 39, SRM 51-21-11 REV 39. ALL WORK PERFORMED UNDER AERSALE WORK ORDER 003854, CARD NO. 20180, TT: 39,453:29 TC: 38,270.
ANGLE BRACKET FOUND CRACKED ON AFT PRESSURE BULKHEAD ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED ANGLE BRACKET ON AFT PRESSURE BULKHEAD FS621, LBL40 REF CRJ200 SRM 51-42-01 REV 39
ANGLE BRACKET FOUND CRACKED ON AFT PRESSURE BULKHEAD ***** AIRCRAFT REMOVED FROM SERVICE ***** REMOVED AND REPLACED ANGLE BRACKET ON AFT PRESSURE BULKHEAD FS621, LBL40 REF CRJ200 SRM 51-42-01 REV 39
ON ARRIVAL AT GATE, NOTICED SMOKE IN CABIN, SMELLS ELECTRICAL. AIRCRAFT REMOVED FROM SERVICE. PERFORMED PACK BURN OUT FOR CLEARING UNUSUAL ORDERS IAW AWA SUP 09-037E. NO DISCREPANCIES NOTED.
RECEIVED IDG 2 CAUTION MULTIPLE TIMES IN FLIGHT. DID NOT RUN QRH MESSAGE CLEARED BELOW 15KFT. R/R BROKEN PIN ON P22EZ IAW ESPM 20-16 OPS CHECK GOOD IAW AMM 24-11
RECEIVED LT AOA HEAT AFTER TAKE-OFF THEN RECEIVED LT PITOT HEAT, LT STATIC HEAT AND PITOT BASE HEAT. PERFORMED QRH AND MESSAGE REMAINED. C/W FIM RESET. SYSTEM OPERATES NORMAL. *******AIRCRAFT REMOVED FROM SERVICE****** NOTED BY MAINTENANCE
AT CRUISE AT FL280, RECEIVED RT ENG OIL PSI WARNING MESSAGE. OIL PSI WAS FLUCTUATING IN THE GREEN BAND. C/W QRH. REDUCED POWER TO IDLE. DIVERTED TO ICT. AROUND 8,000FT, OIL PSI WENT INTO THE RED AND REMAINED THERE FOR THE REST OF THE FLIGHT. SHUT ENGINE DOWN AFTER LANDING. ****AIRCRAFT REMOVED FROM SERVICE**** IN WORK ***SUPPLEMENTAL INFORMATION ****AT CRUISE AT FL280, RECEIVED RT ENG OIL PSI WARNING MESSAGE. OIL PSI WAS FLUCTUATING IN THE GREEN BAND. C/W QRH. REDUCED POWER TO IDLE. DIVERTED TO ICT. AROUND 8,000FT, OIL PSI WENT INTO THE RED AND REMAINED THERE FOR THE REST OF THE FLIGHT. SHUT ENGINE DOWN AFTER LANDING. ****AIRCRAFT REMOVED FROM SERVICE**** R&R RH ENG IAW MTCM SUPP 12-11. ALL RII AND CKS REF TASK CARD 000-71-400-003AW.
R/H WING FLIGHT SPOILER AT WS 264 HAS A CRACKED SEAL P/N: 601R10226-130 JUST BENEATH FWD EDGE OF SPOILER ON WING. CRACK DIMENSIONS ARE 6.5"L X .050"W. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH CRACKED SEAL P/N: 601R10226-130 AT R/H FLIGHT SPOILER WS 264 IAW CRJ200 SRM 51-42-06 REV 39. RESTORED PROTECTIVE FINISH TO R/H WING SEAL IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20196. CRS #4AER685B N444ZWW TT: 38,791:53 TC: 37,500
L/H FLOOR SEAT TRACK FROM FS 364 TO FS 409+128 LBL 9 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON L/H FLOOR SEAT TRACK AT FS 364 TO FS409+128 AND LBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH L/H FLOOR SEAT TRACK FROM FS 364 TO FS 409+128 LBL 9 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACK PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39, AND CRJ200 SRM 51-25-01 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20255. CRS #4AER685B N444ZW TT: 38,791:53 TC: 37,500
R/H FLOOR SEAT TRACK FROM FS 559+80 TO FS 559+96 RBL 27 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H FLOOR SEAT TRACK AT FS 559+80 TO FS 559+96 AND RBL 27 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-51-49 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH R/H FLOOR SEAT TRACK FROM FS559+80 TO FS559+96 RBL 27 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACK PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39, AND CRJ200 SRM 51-25-01 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20277. CRS #4AER685B N444ZW TT: 38,791:53 TC: 37,500
R/H SIDEWALL SEAT TRACK FROM FS 349 TO FS 409 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H SIDEWALL SEAT TRACK AT FS 349 TO FS 409 AND RBL 46 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH R/H SIDEWALL SEAT TRACKS FROM FS 349 TO FS 409 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACKS PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39, AND CRJ200 SRM 51-25-01 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20201. CRS #4AER685B N444ZW TT: 38,791:53 TC: 37,500
L/H FLOOR SEAT TRACK FROM FS 559+80 TO FS 559+96 LBL 27 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON L/H FLOOR SEAT TRACK AT FS 559+80 TO FS 559+96 AND LBL 27 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-51-49 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH L/H FLOOR SEAT TRACK FROM FS559+80 TO FS559+96 LBL 27 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACK PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39, AND CRJ200 SRM 51-25-01 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20274. CRS #4AER685B N444ZW TT: 38,791:53 TC: 37,500
L/H FLOOR SEAT TRACK FROM FS 559+87 TO FS 559+96 LBL 9 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON L/H FLOOR SEAT TRACK AT FS 559+87 TO FS 559+96 AND LBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-51-49 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH L/H FLOOR SEAT TRACK FROM FS 559+87 TO FS559+96 LBL 9 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACK PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39, AND CRJ200 SRM 51-25-01 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20275. CRS #4AER685B N444ZW TT: 38,791:53 TC: 37,500
CORROSION ON R/H FLOOR STRAP P/N: 601R31025-29 AT FS 559.00+32 AND RBL 27 TO RBL 36. ******************AIRCRAFT REMOVED FROM SERVICE********************** BLENDED 2 EACH AREAS ON R/H FLOOR STRAP P/N: 601R31025-29 AT FS 559.00+32: (P1) = 4.5"L X 2.0"W X .019"D (RBL 30) AND (P2) = 2.0"L X 1.5"W X .015"D (RBL 32) AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-00 REV 39. FABRICATED REPLACEMENT STRAP OUT OF 7075-T6 .050" IAW CRJ200 SRM 53-41-43 REV 39, CRJ200 SRM 53-41-43 REV 39, AND CRJ200 SRM 51-24-21 REV 39. APPLIED PROTECTIVE AND DECORATIVE FINISH ON FABRICATED FLOOR STRAP IAW CRJ200 SRM 51-21-11 REV 39 AND CRJ 200 SRM 51-25-01 REV 39. REMOVED AND REPLACED R/H FLOOR STRAP P/N: 601R31025-29 IAW CRJ200 SRM 51-42-06 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20259 AT AERSALE CRS #4AER685B. N444ZW TT:38,791:53 TC:37,500
R/H FLOOR SEAT TRACK FROM FS 559+87 TO FS 559+96 RBL 9 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H FLOOR SEAT TRACK AT FS 559+87 TO FS 559+96 AND RBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-51-49 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH R/H FLOOR SEAT TRACK FROM FS559+87 TO FS559+96 RBL 9 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACK PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39, AND CRJ200 SRM 51-25-01 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20276. CRS #4AER685B N444ZW TT: 38,791:53 TC: 37,500
R/H FLOOR SEAT TRACK FROM FS 364 TO FS 409 RBL 9 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H FLOOR SEAT TRACK AT FS 364 TO FS 409 AND RBL 9 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-21-49 REV 39. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH R/H FLOOR SEAT TRACK FROM FS 364 TO FS 409 RBL 9 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACK PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 39, CRJ200 SRM 51-25-06 REV 39, AND CRJ200 SRM 51-25-01 REV 39. WORK COMPLETED ON AERSALE WO #003644 CARD #20254. CRS #4AER685B N444ZW TT: 38,791:53 TC: 37,500
L/H #1 ENGINE BRACKET P/N:228-50020-805 CRACKED AT 7 O'CLOCK POSITION AND BRACKET P/N: 228-50020-161 CRACKED AT 11-12 O'CLOCK POSITON ON NOSE INLET ATTACH RING. L/H #1 ENGINE NOSE COWL ATTACH RING FLANGE HAS 2 EA ELONGATED HOLES AT 7 O'CLOCK POSITION AND BETWEEN 11 TO 12 O'CLOCK POSITION. ******AIRCRAFT REMOVED FROM SERVICE****** REMOVED L/H #1 ENGINE BRACKET P/N: 228-50020-805 (7 O'CLOCK) POSITION AND BRACKET P/N: 228-50020-161 (11-12 O'CLOCK) POSITION. UPON REMOVAL OF L/H #1 ENGINE NOSE COWL ATTACH RING BRACKETS FOUND 2 EACH DAMAGED HOLES UNDER EACH REMOVED BRACKET. MEASURED HOLE DAMAGE AT EACH LOCATION: 11-12 O'CLOCK (P1) DIMENSION IS 0.245"(L) X 0.125"(W); 7 O'CLOCK (P2) DIMENSION IS 0.308"(L) X 0.286"(W). OPENED HOLE AT (P1) TO 0.2500" DIAMETER AND (P2) TO 0.3080" DIAMETER. HFEC INSPECTION PERFORMED AT AND AROUND BOTH HOLE LOCATIONS WITH NO INDICATIONS FOUND IAW CRJ200 NDT MANUAL PART 1 51-20-06 REV 43. MANUFACTURED (P1) FREEZE PLUG P/N: 601R-71-61-4348-1 (.2509 DIA) AND FREEZE PLUG P/N: 601R-71-61-4348-2 (.3089 DIA) OUT OF 7075-T6 BAR QQ-A-225/9. INSTALLED FREEZE PLUGS AT (P1) AND (P2) HOLE LOCATIONS. DRILLED .128" HOLE THROUGH FREEZE PLUG AT (P1) AND (P2) HOLE LOCATION MAINTAINING 0.050" WALL THICKNESS IN FREEZE PLUG. RESTORED SURFACE FINISH TO (P1) AND (P2) HOLE LOCATIONS.
L/H SIDEWALL SEAT TRACK FROM FS 409+16 TO FS 409+112 HAS SEVERAL AREAS SURFACE CORROSION. EVALUATED CORROSION ON L/H SIDEWALL SEAT TRACK AT FS 409+16 TO FS 409+112 AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-49 REV 38. *********AIRCRAFT REMOVED FROM SERVICE*************************** REMOVED AND REPLACED 1 EACH L/H SIDEWALL SEAT TRACKS FROM FS 409+16 TO FS 409+112 IAW CRJ200 AMM 53-01-11 REV 65. RESTORED PROTECTIVE FINISH TO SEAT TRACKS PRIOR TO INSTALLATION IAW CRJ200 SRM 51-21-11 REV 38, CRJ200 SRM 51-25-06 REV 38, AND CRJ200 SRM 51-25-00 REV 38. WORK COMPLETED ON AERSALE WO #003644 CARD #20199. CRS #4AER685B N444ZWW TT: 38,791:53 TC: 37,500
R/H AFT LOWER SKIN IS DENTED AND HAS SCRATCHED ON FS 589 - FS 605 AT S-24R TO S-25R. ****AIRCRAFT REMOVED FROM SERVICE ***** INSTALLED REPAIR DOUBLER, TRIPLER, AND FILLER TO REPAIR AREA ON AIRCRAFT SKIN EXTERIOR IAW ASAP EA #AWAC-CRJ253-01860 REV IR DATED 07-15-2022. RESTORED PROTECTIVE/DECORATIVE FINISH TO AIRCRAFT SKIN EXTERIOR REPAIR/REPAIR PARTS IAW ASAP EA #AWAC-CRJ253-01860 REV IR DATED 07-15-2022. IDENTIFIED REPAIR WITH INDELIBLE INK AS ASAP EA #AWAC-CRJ253-01860 IAW ASAP EA #AWAC-CRJ253-01860 REV IR DATED 07-15-2022. ALL WORK PERFORMED WITHIN ALLOWABLE LIMITS IAW ASAP EA #AWAC-CRJ253-01860 REV IR DATED 07-15-2022. WORK COMPLETED ON AERSALE WO #003644 CARD #20050. N444ZW TT:38,791:53 TC:37,500
L 14TH BLEED AIR WARNING FREQUENTLY CLIMBING THRU 20,000FT ONCE EVERY 3 SECONDS, C/W QRH BROUGHT ENG TO IDLE. MSG CONTINUED 1 EVERY MINUTE. STOPPED WHEN ENG SHUT DOWMN ON GROUND. (BK 4) SNYOPTIC SHOWED RED BETWEEN 14TH SATGE SOC, MSOV AND COWL SOV. ALSO RECEIVED BLEED AIR DUCT AURAL WARNING. ***AIRCRAFT REMOVED FROM SERVICE*** MX IN PROGRESS
L 14TH BLEED AIR WARNING FREQUENTLY CLIMBING THRU 20,000FT ONCE EVERY 3 SECONDS, C/W QRH BROUGHT ENG TO IDLE. MSG CONTINUED 1 EVERY MINUTE. STOPPED WHEN ENG SHUT DOWMN ON GROUND. (BK 4) SNYOPTIC SHOWED RED BETWEEN 14TH SATGE SOC, MSOV AND COWL SOV. ALSO RECEIVED BLEED AIR DUCT AURAL WARNING. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED LH ENGINE 14TH STAGE BLEED AIR LEAK TEST WITH ENGINES BLEED AIR IAW AMM 36-12-00 FOUND LH 14TH SOV AND LH AICE CLAMPS LOOSE. RE TIGHTENED LOOSE CLAMPS IAW AWAC SUP 10-008, NO LEAKS NOTED AT THE TIME. ALSO PERFORMED LH BLEED AIR LEAK OPERATIONAL CHECK IAW AMM 36-21-10, OPS CHECK GOOD.
CLIMBING THROUGH 7000 RH ENG ITT 888 FLASH RED AT N1 87% AFTER APPROXIMATELY 10 SEC HEARD BANG AND SHUTTER. A/C YAWED AS RH, ENG POWER REDUCED. ACCOMPLISHED ENG SHUTDOWN. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED R/H ENGINE S/N 872452 OFF WITH S/N 872307 ON REF WO 300993 FOR ALL MAINT PERTAINING TO R&R OF RH ENGINE. ALL GRND RUNS AND LEAK CHECKS GOOD.
3 EA PROTRUDING DENTS IN AFT FUSELAGE SKIN AT FS 682.00 BETWEEN STR 23R AND STR 24R. AIRCRAFT REMOVED FROM SERVICE. CUTOUT DAMAGE AREA AT FS 672 TO FS 682 BETWEEN STR 23R AND STR 24R, REF CRJ200 SRM 53-00-31 REV 38. PERFORMED HFEC INSPECTION AROUND CUTOUT AREA AT FS 672 TO FS 682 BETWEEN STR 23R TO STR 24R, REF CRJ 200 NDTM PART 1 EDDY-CURRENT INSPECTION PROCEDURES 51-30-06 REV 41. FABRICATED REPAIR DOUBLER FROM ALUMINUM SHEET 2024-T3, 0.063" AT FS 672 TO FS 682 BETWEEN STR 23R TO STR 24R. REPAIR DOUBLER L=12.200", W=8.500", REF CRJ 200 SRM 53-00-31 REV 38.
FS 441 & RBL 42 HAS CORROSION ON FLOOR SILL PANEL AT NUTPLATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR SILL PANEL AT FS 441 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 1.067" L X 1.414" W X .003" D. PERFORMED HFEC NO INDICATIONS NOTED, REF NDTM PART 1 51-20-06 REV 41. TREATED, PRIMED, PAINTED, AND APPLIED CPC, REF BOMBARDIER REO 601R-53-41-666 REV C DTD 2012-11-06.
CORROSION ON FLOOR ANGLE AT STATION 517, RBL 39, TO RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 517 RBL 39 TO RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=2.000" W=1.800" D=0.007" ORIGINAL THICKNESS 0.080" REMAINING THICKNESS IS 0.073", REF CRJ 200 SRM 53-41-45. REWORKED AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.
CORROSION ON FLOOR ANGLE AT STATION 447,AND RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 447 AND RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=1.920" W=1.400" D=0.007" ORIGINAL THICKNESS 0.080" REMAINING THICKNESS AFTER REWORK IS 0.073', REF CRJ 200 SRM 53-41-45. REWORK AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.
CORROSION ON FLOOR ANGLE AT FS 500 TO FS 513 RBL 47. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT FS 500 TO FS 503 AND BL 47, REF CRJ 200 SRM 51-21-06. REWORKED AREA MEASURES 1.6" L X 0.9" W X .006 D. ORIGINAL MATERIAL THICKNESS .080", REMAINING MATERIAL THICKNESS .074". HFEC INSPECTION ACCOMPLISHED WITH NO INDICATION NOTED, REF NDTM PART 1 51-20-06 REV 41. TREATED, PRIMED, PAINTED, AND APPLIED CPC WITHIN ALLOWABLE LIMITS, REF BOMBARDIER REO 601R-53-41-666 REV C DTD 2012-11-06.
FLOOR SILL PANEL AT FS 441 & RBL 42 AROUND NUTPLATE HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR SILL PANEL AT FS 441 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 1.067" L X 1.414" W X .003" D. PERFORMED HFEC, NO INDICATIONS NOTED, REF NDTM PART 1 51-20-06 REV 41. TREATED, PRIMED, PAINTED, AND APPLIED CPC, REF BOMBARDIER REO 601R-53-41-666 REV C DTD 2012-11-06.
CORROSION ON FLOOR ANGLE AT STATION 468, TO STATION 470, LBL 40. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT STATION 468 TO STATION 470, REF CRJ 200 SRM 53-41-06. MEASURE OF REWORK AREA L=3.500" W=I.400" D=0.006" ORIGINAL THICKNESS 0.080" REMAINING THICKNESS AFTER REWORK 0.740", REF CRJ 200 SRM 53-41-45. REWORK AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.
CORROSION ON FLOOR ANGLE AT FS 448 TO FS 451 AND RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT FS 448 TO FS 451 RBL 42, REF CRJ 200 SRM 51-21-06. REWORKED AREA MEASURES 1.80" L X 0.95" W X .003" D. ORIGINAL MATERIAL THICKNESS .080" REMAINING THICKNESS .077". HFEC INSPECTION ACCOMPLISHES WITH NO INDICATIONS NOTED, REF NDTM PART 1 51-20-06 REV 41. TREATED, PAINTED, AND APPLIED CPC WITHIN ALLOWABLE LIMITS, REF BOMBARDIER REO 601R-53-41-666 REV C DTD 2012-11-06.
CORROSION ON PRESSURE FLOOR SILL AT STATION 447, AND LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON PRESSURE FLOOR SILL AT STATION 447, AND LBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=1.141" W=0.883" D=0.006", ORIGINAL THICKNESS IS 0.055", REF CRJ 200 53-41-45. REMAINING THICKNESS IS 0.049", REWORKED AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.
CORROSION ON FLOOR ANGLE AT STATION 461.50 & RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 461.50, & RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=0.900" W=0.950" D=0.003", ORIGINAL THICKNESS 0.080", REMAINING THICKNESS AFTER REWORK TO BE 0.077", REF CRJ 200 SRM 53-41-45. REWORK AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.
CORROSION ON FLOOR ANGLE AT STATION 508, LBL 36 TO 38. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT STATION 508, TO STATION 510, LBL 36, TO LBL 38, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=1.702" W=1.643" D=0.006", ORIGINAL THICKNESS 0.080", REMAINING THICKNESS AFTER REWORK IS 0.074", REF CRJ 200 SRM 53-41-45. REWORKED AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.
CORROSION ON FLOOR ANGEL AT STATION 438 TO STATION 439 RBL 40C. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT STATION 439, TO 439 & RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=1.377" W=0.390" D=0.003", ORIGINAL THICKNESS 0.080", REMAINING THICKNESS IS 0.077", REF CRJ 200 SRM 53-41-45. REWORKED AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) NR 601R-53-41-666 REV C DATED, 2012-11-06.
CORROSION ON FLOOR ANGLE AT STATION 469, RBL 36. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 469, RBL 36, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=1.373" W=0.961" D=0.011", ORIGINAL THICKNESS IS 0.080". REMAINING THICKNESS IS 0.069" REWORKED AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.
FS 541 & RBL 42 HAS CORROSION ON FLOOR SILL PANEL AT NUTPLATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR SILL PANEL AT FS 541 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORK AREA MEASURES 1.267" L X 1.006" W X .004" D. PERFORMED HFEC NO INDICATIONS NOTED, REF NDTM PART 1 51-20-06 REV 41. TREATED, PRIMED, PAINTED, AND APPLIED CPC, REF BOMBARDIER REO 601R-53-41-666 REV C DTD 2012-11-06.
CORROSION ON FLOOR ANGLE FS 523 TO FS 530, RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT FS 523 TO FS 530 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORKED AREA MEASURES 2.5" L X 1.40" W X .006" D. ORIGINAL MATERIAL THICKNESS .080", REMAINING MATERIAL THICKNESS .074". HFEC ACCOMPLISHED WITH NO INDICATIONS NOTED, REF NDTM 51-20-06, PART 1, REV 41. TREATED, PRIMED, PAINTED AND APPLIED CPC. WITHIN ALLOWED LIMITS, REF BOMBARDIER REO 601R-53-41-666, REV C, 2012-11-06.
CORROSION ON FLOOR ANGLE AT STATION 468 & RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGLE AT STATION 461.50, & RBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORKED AREA L=0.900" W=0.950" D=0.013" ORIGINAL THICKNESS 0.080" REMAINING THICKNESS AFTER REWORK TO BE 0.067", REF CRJ 200 SRM 53-41-45. REWORK AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.
CORROSION AT NUT PLATE ON FLOOR SILL PANEL FS 522 RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT FS 522 & RBL 42 AT NUT PLATE ON FLOOR SILL, REF CRJ 200 SRM 51-21-06. REWORKED ARE MEASURES .925" L X .912" W X .005" D. ORIGINAL MATERIAL THICKNESS .055", REMAINING MATERIAL THICKNESS .050". HFEC ACCOMPLISHED WITH NO INDICATIONS NOTED, REF NDTM 51-20-06, PART 1, REV 41. TREATED, PRIMED, PAINTED AND APPLIED CPC. WITHIN ALLOWED LIMITS, REF BOMBARDIER 601R-53-41-666, REV C, 2012-11-06.
CORROSION ON FLOOR SILL PANEL STATION 467, AND LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR SILL PANEL AT STATION 467, AND LBL 42, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=0.950" W=0.780" D=0.006", ORIGINAL THICKNESS 0.055", REF CRJ 200, SRM 53-41-45. REMAINING THICKNESS AFTER REWORK IS 0.490", REWORK AREA FOUND TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.
CORROSION ON FLOOR ANGLE AT FS 484 & RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION AT RT FLOOR ANGLE AT FS 484 & RBL 42, REF CRJ 200 SRM 51-21-06. REWORKED AREA MEASURES 1.96" L X 1.44" W X .005" D, ORIGINAL MATERIAL THICKNESS .080", REMAINING MATERIAL THICKNESS .075". HFEC ACCOMPLISHED WITH NO INDICATIONS NOTED, REF NDTM PART 1 51-20-06 REV 41. TREATED, PRIMED, PAINTED, AND APPLIED CPC. WITHIN ALLOWABLE LIMIT,S REF BOMBARDIER REO 601R-53-41-41-666 REV C 2012-11-06.
CORROSION ON FLOOR ANGEL AT STATION 517, LBL 36, TO LBL 37. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FLOOR ANGEL AT STATION 517, LBL 36, LBL 37, REF CRJ 200 SRM 51-21-06. MEASURE OF REWORK AREA L=0.851" W=0.080" D=0.005", ORIGINAL THICKNESS 0.080", REMAINING THICKNESS IS 0.075", REF CRJ 200 SRM 53-41-45. FOUND REWORKED AREA TO BE WITHIN LIMITS, REF REPAIR ENGINEERING ORDER (REO) 601R-53-41-666 REV C DATED 2012-11-06.
APB FS 621 IS PUNCTURED JUST ABOVE FLOOR AT LBL 24.0 REPAIRED APB FS 621 JUST ABOVE FLOOR LBL 24 IAW BOMBARIDER REO# 601R-53-61-6673 REV --
AFT PRESSURE BULKHEAD HAD A CRACK AT THE LINTEL FITTING. REPAIRED THE AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1230, REV F, AND REO 601R-53-61-6671 REV -.
AFT PRESSURE BULKHEAD WAS CRACKED AT THE AFT CARGO DOOR TRACK, LBL 27.5, WL 125. REPAIRED THE AFT PRESSURE BULKHEAD IAW REO 601R-53-61-1541 REV-F.
VERTICAL STAB, AFT FRAME UNDER PANEL 326AT HAD A DAMAGED SCREW HOLE. REPAIRED THE VERTICAL STAB AFT FRAME IAW EA CRJ255-01022, REV-IR.
PAX DOOR ELECTRICAL CONNECTOR FITTING FOR P2MB, AT THE LOWER SILL WAS CORRODED AND CRACKED. REPLACED THE FITTING.
FLOORBEAM OTBD ANGLE AT BS 280, LBL 9 WAS CRACKED. REPLACED THE ANGLE.
FLOORBEAM INBD ANGLE AT BS 280, LBL 9 WAS CRACKED. REPLACED THE ANGLE.
FLOORBEAM OTBD ANGLE AT BS 280, RBL 9 WAS CRACKED. REPLACED THE FLOORBEAM ANGLE.
RIGHT OTBD FLAP FITTING AT FLAP STATION 280.66 WAS WORN TO LIMITS. REPLACED.
BS 280 FLOORBEAM WEB LWR AFT ANGLE AT LBL 12 WAS CRACKED. REPAIRED THE FLOORBEAM.
RIGHT INBD FLAP, LOWER INBD SKIN HAD NUMEROUS ROCK PITS. REPLACED THE FLAP.
LEFT INBD FLAP VANE LEADING EDGE WAS CHAFED AT WS 104.0. REPLACED THE FLAP VANE.
LH WING TRAILING EDGE RIB AT WS 130.10 WAS CRACKED. REPLACED THE RIB.
FLOORBEAM INBD ANGLE CRACKED AT BS 280, RBL 9. REPLACED THE ANGLE IAW SRM 51-21-43, 51-31-59, 51-24-36, AND 51-41-21.
PANEL 422AT SEAL RETAINER CRACKED. REPLACED SEAL RETAINER IAW SRM 51-42-06.
BS 280 FLOORBEAM WAS CRACKED AT RBL 9. REPLACED THE FLOORBEAM IAW SRM 51-42-06.
AFT PRESSURE BULKHEAD FWD FACE AT BL0 HAS 2 CRACKS 38 IN AND 57 IN ABOVE FLOOR.
CARGO DOOR STEP PLATE WAS CRACKED. REPLACED THE STEP PLATE IAW SRM 51-40-11.
FLOORBEAM STRAP CORRODED AT BS 559, RBL 27 TO RBL 43. REPLACED THE STRAP IAW SRM 51-42-06, 53-00-00, AND 53-41-43.
BS 484 FLOORBEAM ANGLE WAS CRACKED AT LBL 36. REPLACED THE FLOORBEAM ANGLE IAW REO 601R-53-41-059, REV-B.
BS 484 FLOORBEAM ANGLE WAS CRACKED AT LBL 27. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-26.
9898 UNCOMMANDED YAW IN CLIMB RUDDER TRIMMED RIGHT MANUALLY CENTERED THEN RUDDER TRIMMED LEFT MANUALLY RE-CENTERED THEN RUDDER WAS UNCONTROLLABLE C/W QRH DISCONNECTED RUDDER A/P OFF ABLE TO CONTROL A/C. NUMEROUS ERRORS ON FCC 1 IN FCC DIAGNOSTICS, R/R FCC 1 IAW AMM 22-22-14 OPS CHECK GOOD, PERFORMED SPIN TEST OF YAW DAMPER PER AMM 22-22-01 OPS CHECK GOOD
FLT. 4007. GEAR DISAGREE AND NOSE GEAR DOOR OPEN WARNING MESSAGES ON DEPARTURE WHEN GEAR LEVER SELECTED UP. LEVER WAS NOT MOVED WITHIN 30 SECONDS OF ORIGINAL SELECTION. NOSE GEAR SHOWED GREEN DOWN AND LOCK MAINS SHOWED YELLOW WITH HASHES THEN SHOWED UP AND LOCKED. MANUAL RELEASE SYSTEN WAS OPERATED. ICING CONDITIONS WERE ENCOUNTERED WITH GEAR EXTENDED. EMERGENCY LANDING DECLARED MAX AIRSPEED WITH GEAR EXTENDED WAS APRROXIMATELY 200 KNOTS, LANDING WEIGHT WAS 41,500 LBS NO HARD LANDING NOTED. JACKED ACFT IAW AMM 07-11-01. NLG STRUT WOULD NOT FULLY EXTEND. STRUT SERVICING REQ. SERVICED NLG STRUT WITH OIL AND NITROGEN IAW 12-12-32-610-803. STRUT FULLY EXTENDS. PERFORMED GEAR SWINGS. OPS CHECKED GOOD.
APU AUTO SHUTDOWN. FOLLOWED BY SMOKE COMING FROM APU INTAKE.
UNCOMMANDED YAW AT FL210, INITIAL ROLL TO THE RIGHT THEN PULSED BACK AND FORTH GENTLY. RAN IAC AND QRH, PROBLEM DISCONTINUED WHEN YAW DAMPER DISCONNECTED
LEFT LOWER FUSELAGE SKIN HAS DENT AT FS 621.00 AND STR 19L. REPAIRED LT LOWER FUSELAGE SKIN AT FS 621.00 AND STR 19L IAW EA CRJ253-0430, REV IR DATED 07/09/2016.
INTERCOSTAL THAT SITS ON TOP OF STR 20L HAS CORROSION BETWEEN FRAME 333.00 AND 349.00 IN THE FWD ELECTRONIC EQUIPMENT BAY. REPLACED INTERCOSTAL ON STR 20L BETWEEN FRAME 333.00 AND 349.00 IAW SRM 51-42-06, 51-42-21. REPAIRED STR 20L IAW EA AWAC-CRJ253-00442, REV-IR DATED 07/13/2016.
STRINGER 26L HAS CORROSION BETWEEN FS 349.00 AND FS 364.00. REPAIRED STRINGER IAW SRM 53-00-03.
INBD FLOOR LANDING ON LBL27 HAS CORROSION AND BARE METAL SPOTS BETWEEN FS 574.00 AND FS 621.00 IN THE CARGO BAY. REPAIRED INBD FLOOR LANDING ON LBL27 FROM FS 574.00 TO FS 605.00 IAW SRM 53-61-43, 53-00-00, 51-31-59. REPAIRED INBD FLOOR LANDING ON LBL 27 FROM FS 605.00 TO FS 621.00 IAW EA CRJ253-00436, REV-IR DATED 07/04/2016.
APU ENCLOSURE BOTH INTERNAL UPPER STIFFENERS WELDS ARE CRACKED AT AFT FLANGE FORWARD SIDE. REPAIRED APU ENCLOSURE INTERNAL UPPER STIFFENERS IAW SUP: 16-168 AND EA CRJ249-00441 AND SUP: 16-206.
PASSENGER DOOR OUTER SKIN CHAFED UNDER HINGE PIN TRAVEL AREA BOTH FORWARD AND AFT CORNERS. FOUND DURING EVALUATION OF SKIN DAMAGES FS 310 AND FS 349.
AFT EQUIPMENT COMPARTMENT FS 621, BULKHEAD LT SKIN ATTACH ANGLE AT STR 14L CRACKED.
AFT EQUIPMENT COMPARTMENT FS 621 BULKHEAD RT OBLIQUE ANGLE AT STR 14R CRACKED.
AFT EQUIPMENT COMPARTMENT FS 621 BULKHEAD LT OBLIQUE ATTACH ANGLE AT STR 14L IS CRACKED.
PASSENGER DOOR HAS A CRACK ON THE AFT WEB UNDER THE AFT DRAG ANGLE. REPAIRED CRACK IAW SUP: 15-310.
WINDSHIELD CENTER POST LT LOWER CLIP IS CRACKED. REPLACED WINDSHIELD CENTER POST LOWER LT CLIP IAW SRM 51-42-21.
AFT EQUIPMENT COMPARTMENT FS 621.00 BULKHEAD LT ANGLE AT STR 16L IS CRACKED. REPLACED ANGLE ON FS 621.00 BULKHEAD AT STR 16L IAW SRM 51-42-21.
FUSELAGE SKIN HAS SCRATCHES ON THE OTBD SIDE, AT THE LOWER FORWARD CORNER OF THE PASSENGER DOOR CUTOUT AT FS 310.00. REPAIRED FUSELAGE SKIN IAW SUP 16-201, DATED 07/06/2016.
FUSELAGE SKIN HAS A SCRATCH ON THE OTBD SIDE AT THE LOWER AFT PASSENGER DOOR CUTOUT AT FS 349.00. REPAIRED FUSELAGE SKIN IAW SUP: 16-201 DATED 07/06/2016.
PASSENGER DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED PASSENGER DOOR AFT DRAG ANGLE IAW GREO 601R-52-11-513, REV B DATED 2015-07-05.
RIGHT LOWER DIVIDER PANEL 422DB HAS A CRACKED FWD DIVIDER. REPLACED LOWER DIVIDER FROM PANEL 422DB IAW SRM 51-42-06.
RIGHT T/R PDU WIRE HARNESS BRACKET IS CRACKED. REPLACED BRACKET IAW SRM 51-42-06.
NR 2 ENGINE EXAHUST FAIRING ATTACHMENT NUT PLATES HAVE CRACKED CLIPS. REPLACED NUT PLATE CLIPS IAW CMM 20-42-06.
LEFT JET PIPE FAIRING HAS CRACKED DOUBLERS AT NUTPLATES FOR ACCESS PANELS. REPLACED THE JET PIPE DOUBLERS IAW CMM 20-42-06.
CARGO TRACK HAS CORROSION AT LBL9 BETWEEN BS 559+112 AND 574, IN THE CARGO BAY. REPLACED THE CARGO TRACK IAW REO 601R-53-00-485 REV-B & AMM 53-00-49.
LEFT WINDSHIELD SIDE POST SUPPORT, LOWER ATTACH ANGLE BELOW WINDOW LINE IS CRACKED. REPLACED THE ANGLE IAW SRM 51-42-06.
PAX DOOR FRAME, NDT VERIFIED CRACKS IN STRINGER 3L AT ATTACH POINT TO AFT UPPER FRAME. REPAIRED THE STRINGER IAW SRM 53-00-03 FIG. 202 SHEET 1.
RIGHT WINDSHIELD SIDE POST SUPPORT, O/B FITTING IS CRACKED. REPLACED RT O/B SIDE POST SUPPORT FITTING IAW SRM 51-42-21.
CARGO DOOR OPENING FLOOR SUPPORT IS CRACKED BETWEEN RIVET AND INNER EDGE AT BS 589. REPAIRED FLOOR SUPPORT IAW REO 601R-53-61-433.
FWD FACE AREA OF THE BS 409 FRAME HAS CORROSION BETWEEN STRINGERS 26 - 27L. REPAIRED AREA IAW SRM 51-42-06, 51-42-21, 51-40-11, AND 51-24-21.
SERVICE DOOR WILL NOT OPEN FROM OUTSIDE.
UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE, HANDLE WON'T POP OUT. DOOR OPENS NORMALLY FROM INSIDE.
COVER FOR FLOOR EMER LIGHTS AT ROW 1 CAME OFF.
AFTER TAKEOFF & GEAR UP, RECEIVED, STEERING INOPERATIVE, CAUTION MSG. COMPLIED WITH QRH, MSG PERSISTS. MSG WENT OUT ON GEAR EXTENSION.
FLIGHT 4021 REF 274230 1, TAPE APPLIED TO FLOOR TRACK LIGHTING STRIP AT ROW 1 IAW GMM CHPT 23. APPROVED FOR ONE FLIGHT. PLACED ON DIL. INSTALLED NEW EMER LIGHT STRIP END CAP IAW AMM 33-51-01. THIS CLEARS DIL.
FLIGHT NR 3746, FLOOR LEVEL EMER LIGHTS INOPERATIVE ROW 7 & AFT. PULLED UP EMER LIGHTING STRIP, INSPECTED WIRING. FOUND WIRE BROKEN AT J 6LY & P7LY. REINSTALLED STRIP FOR FERRY IAW AMM 33-51-01.
FLIGHT 3849. 3845, 3849, & 3983 EMER LIGHT STRIP 1ST SEGMENT AT ROW 1 PULLED UNLIT. SECURED LIGHTING STRIP WIRES & FLOOR TRACK IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.
FLIGHT NR 4004, ON FIRST ATTEMPT TO START THE APU THE DOOR DID NOT OPEN, ON SECOND ATTEMPT THE DOOR OPENED BUT THE RPM HUNG 28% & A STRONG FUEL ODOR FILLED THE CABIN. COMPLIED WITH CM ACTION PLACARDED & PLACED ON MEL. R & R APU ECU IAW AMM 49-61-01. OPERATIONS CHECKED GOOD. REMOVED PLACARD & REMOVED FROM MEL.
CAPTAIN`S WINDSHIELD SHATTERED AT APPROX 14,000 FT. CREW STOPPED CLIMB & CONTACTED ATC. EMER DECLARED. INSPECTED & FOUND THE OUTER PLY TO BE CRACKED, REF SUPP 14-201A. R & R CAPTAIN'S WINDSHIELD & PERFORMED WINDSHIELD HEAT CHECK & LEAK CHECK IAW AMM 56-11-01. NOTE, CHECKED GOOD. IAW 269609 3 RESET CBS CB P1-G5 G6, F12, A10 & A11. OPERATIONS CHECKED CHECK GOOD.
FLIGHT ATTENDANT SMELLED ELEC BURNING SMELL. IN THE GALLEY AREA SMELLED THE STRONGEST COMPARED TO THE REST OF THE CABIN, WHILE LIGHTS WERE ON DIM.
CARGO DOOR HANDLE HOUSING IS CRACKED.
RIGHT INBD FLAP INBD HINGE ARM FAIRING GUIDE PLATE SUPPORT STRUCTURE ON FWD SIDE OF HINGE ARM IS CRACKED.
LOWER U BRACKET CRACKED AT RIVET FS 574.00.
PYLON PNL 422BT SEAL RETAINER IS CRACKED.
FS 349 FRAME IN AVIONICS BAY HAS CORROSION.
RT WING INBD FLAP, INBD HINGE BOX, AFT ATTACHMENT FITTING IS GOUGED.
LBL 27 CORRODED ON TOP SURFACE AT RS 621.00.
MLG TRUNNION LWR FLANGES FOUND TWO EACH OS HOLES 1LT & 1RT.
LEFT OTBD FLAP CTR HINGE ARM SHROUD PLATE IS CRACKED.
PYLON PNL 412DB SEAL RETAINER IS CRACKED.
RT MLG DRAG ANGLE COMMON TO BATTERY RIB IS CRACKED.
RT MLG BRAKE PRESS TRANSDUCER FWD BRACKET CRACKED.
CARGO DOOR SUPPORT BEAM AFT LOWER CLIP IS CRACKED.
CARGO FLOOR TRACK CORRODED AT FS 574 RBL 9.
UPPER BRAKE ACCUMULATOR BRACKET IS CRACKED.
NR 2 HYD ACCUMULATOR MOUNT BRACKET IN AEB IS CRACKED.
RT LOWER NOSE COWL TORQUE BOX SPRING SEAL IS CRACKED.
LT MLG DRAG ANGLE COMMON TO BATTERY RIB CRACKED.
RBL 27 FLOORBEAM CAP OTBD FLANGE GOUGED NEAR RIVET.
FS 484 CLIP CRACKED AT LBL 27.
FS 484 CLIPS CRACKED AT RBL 27 & 36.
CARGO BAY PRESS DIAPHRAGM SUPPORT PLATE CORRODED.
RT FLOOR SEAT TRACK CORRODED AT FS 559+24.
LOWER FRAME SECTOR AT FS 319 IS CORRODED FROM STRINGER 26L TO 26R.
LT SIDE SEAT RAIL CORRODED AT FS 417.
LOWER FRAME SECTOR CORRODED AT FS 333 FROM STRINGER 26L TO 26R.
STAB TRIM FAULT AT 2.8 BOTH CHANNELS DISENGAGED, COMPLIED WITH NEITHER CHANNEL WOULD RE-ENGAGE. AUTOPILOT WAS ENGAGED. IAW PG 270843 4 FOR CORRECTIVE ACTION, R & R PILOT'S STAB TRIM DISCONNECT SWITCH. CAPTAIN'S DISCONNECT SWITCH FAILED SENSITIVITY TEST. R & R CAPTAIN`S PITCH TRIM, DISCONNECT SWITCH IAW AMM SUPP 10-048A, OPERATIONS CHECKED GOOD.
FLOORBEAM, FS 280.00 IS CRACKED JUST OTBD OF RBL 9. REPAIRED IAW REO 601R-53-11-2338 BY CUTTING AWAY DAMAGE AND INSTALLING REPAIR ANGLE AND FILLERS.
PAX DOOR STAIR STRUCTURE CRACKED ON AFT SIDE PANEL @ 3RD STEP. REPAIRED PAX DOOR AFT SIDE PANEL @ 3RD STEP IAW REO 601R-52-11-702, REV C.
PAX DOOR AFT DRAG ANGLE IS CRACKED. REMOVED UNSERVICEABLE DRAG ANGLE WITH NEW SERVICEABLE DRAG ANGLE IAW REO 601R-52-11-513, REV A.
PAX DOOR STAIR STRUCTURE IS CRACKED ON FWD SIDE OF 4TH STEP. REPAIRED FWD SIDE PANEL AT 4TH STEP ON PAX DOOR IAW REO 601R-52-11-702.
CARGO DOOR FLOOR SILL HAS CORROSION AROUND SCREW HOLES UPPER LOWER SIDES. REMOVED UNSERVICEABLE CARGO DOOR FLOOR SILL AND REPLACED WITH SERVICEABLE FLOOR SILL PN 60135011-63 IAW SRM 51-42-06, 51-40-11.
PAX DOOR SILL FLOOR SUPPORT STRUCTURE HAS CORROSION. REMOVED PAX DOOR SILL FLOOR SUPPORT ANGLE AND REPLACED WITH SERVICEABLE ANGLE IAW SRM 51-24-21, 51-42-06, 51-42-21.
PAX DOOR AFT CORNER DAMAGED. REPAIRED PAX DOOR AFT CORNER IAW REO 601R-52-11-2066.
PILOTS SIDE POST LOWER FITTING CRACKED. REMOVED UNSERVICEABLE WINDOW POST LOWER FITTING. REPLACED WITH SERVICEABLE FITTING, PN 601R33235-3S.
FLOOR SUPPORT LBL27 IN CARGO AREA HAS CORROSION. REMOVED UNSERVICEABLE LBL27 FLOOR SUPPORT CAP AND INSTALLED SERVICEABLE LBL 27 FLOOR SUPPORT CAP IAW SRM 51-42-06, 51-42-27, REO 601R-53-61-3778, REV A.
LT 9G INBD AND OTBD TIE DOWN TRACKS HAS CORROSION. R & R LT 9G CORRODED TIE DOWN TRACKS IAW AMM 53-01-11.
TWO TIE DOWN TRACKS ON LBL 9 IN CARGO AREA HAS CORROSION. R & R TIE DOWN TRACKS ON LBL 9 IAW AMM 53-01-11.
PRESSURE BULKHEAD FS 202.75 IS GOUGED JUST OTBD OF PARKING BRAKE CONTROL CABLE PASS THRU. REPAIRED BULKHEAD IAW REO 601R-53-11-563, REV B, REPAIR TYPE V.
LEFT JET PIPE HAS SMALL SHARP DENT ON THE TOP SIDE. PERFORMED REPAIR ON LIGHT JET PIPE TOP SIDE IAW CMM 78-11-00.
RIGHT 9G INBD CARGO TRACK HAS CORROSION. R & R RT 9G CARGO TRACK IAW AMM 53-01-11.
DURING FLIGHT IN ICING CONDITIONS, RECEIVED WING OVERHEAT RED WARNING. EICAS INDICATED RT WING L/E RED. C/W QRH, RECEIVED RT-WING OVERHEAT IN STANDBY MODE. R & R RT MODULATING SHUTOFF VALVE IAW AMM 30-12-14 LEAK AND OPS CK GOOD.
SELECTED WING HEAT TO STANDBY IM ICING CONDITIONS AND RECEIVED WING O/H WARNING, LT ICING CONDITIONS AND C/W QRH (RT WING). R & R TEMP CONTROL UNIT IAW AMM 31-12-19. OPS CHECKED GOOD. REMOVED PLACARD AND MEL.
RT WING OVERHEAT MESSAGE IN FLIGHT. SELECTED WING ANTI-ICE OFF. MESSAGE CLEARED WITHIN 5 SEC. DETERMINED RT WING DUCT TO BE AT FAULT SELECTED RT 14TH STAGE ISO OPEN AND WING ANTI-ICE TO STANDBY. R & R LT MODULATING SHUTOFF VALVE.
FOUND WEBBING OTBD OF RBL 9 CRACKED AT FS 559, REPAIRED WEB OF FS 559 PRESSURE BULKHEAD, RT SIDE, RBL 9 TO 18 IAW REO 601R-53-41-1495, REV A.
FOUND LBL 900 OTBD POST CRACKED AT FS 559.0. REPAIRED LBL 9.0 OTBD POST BY FULL INCORPORATION OF REO 601R-53-41-057, REV A.
ON TAKEOFF, AFTER RETRACTING GEAR, GOT GEAR UNSAFE/ NOSE DOOR OPEN WARNING. PERFORMED QRH. NOSE GEAR DID NOT SHOW UP AND LOCKED. EVERYTHING WORKED NORMALLY AFTER GEAR EXTENDED. OPEN
WHILE IN FLT, AC 1 AUTO TRANSFER AC BUS 1 GEN 1 OFF AND LT WINDOW HEAT CAUTION MSG ILLUMINATED ON ED1 CW QRH FLAP .5 SPEED ON ED2 IN FLAP SELECTION OTHER AS MSG. R & R GEN CONTROL UNIT.
LT OTBD FLAP, BUTTE DOOR PANEL NR 594PB HAS MINOR CHAFING. R & R BUTTE DOOR PANEL NR 594PB WITH SERVICEABLE PART PN 601R102279 IAW SRM 51-42-06.
RT OBLIQUE ANGLE IS AEB IS CRACKED. R & R RT OBLIQUE ANGLE BETWEEN FS 621 & FS 625, AT RBL 36, STR 14R IAW SRM 51-42-21.
AFT SIDE OF 280 BULKHEAD AFT FLIGHT DECK CUT OUT ON RT SIDE IS CHAFED IN 2 SPOTS REPAIR IAW REO 601R-53-11-1727, REV C 2009/09/24. REPAIR 1 (WEB REPAIR AND CHANNEL MINOR BLEND OUT).
REQUEST INSPECTION FOR SMOKE ODOR IN REAR OF CABIN NEAR ROW 12. INSPECTED DUCTING, CLEANED AND INSPECTED RT PACK COALERSCER SOCK, INSPECTED PSU ROW 12 RT, NO EVIDENCE OF SMOKE OR ARCING. OPS CHECK GOOD, OK FOR SERVICE.
ON CLIMBOUT, AFTER INITIAL LT TURN, RUDDER (TRIM) RAN FULL LEFT DEFLECTION UNCOMMANDED. ABLE TO OVER POWER WITH USE OF RUDDER PEDAL. AUTO-PILOT WAS NOT ENGAGED. DECLARED EMERGENCY LANDING IN IAD. REMOVED AND REPLACED TRIM CONTROL PANEL AND RUDDER TRIM ACTUATOR. (K)
F/O YOKE CLIP LIGHT BROKEN, SPARKED AND SMOKED INTERMITTENTLY AND NOW CEASED TO WORK. FOUND C/B CBP2 U6 POPPED, PULLED AND COLLARD. INSPECTED YOKE CHART HOLDER DAMAGE NOTED. REF LP 188421/1 FOR CHART HOLDER MEL. (K)
FUEL LEAK BELOW APU. FOUND APU FUEL SUPPLY LINE O-RING DETERIORATED. REMOVED AND REPLACED APU FUEL LINE O-RING IAW AMM 49-31-01-420-001. NO LEAKS. OK FOR SERVICE. (K)
BRACKET OF SERVICE DOOR INNER HANDLE MICRO SWITCH BROKEN. BRACKET OF SERVICE DOOR INNER HANDLE REPLACED. (A)
REPAIR CRACK ON PASSENGER DOOR. PASSENGER DOOR EDGE MEMBER REPAIRED IAW CRJ 200 REO 601R-53-11-279. (A)
CARGO STOW PLATE HINGES (3) CRACKED. CARGO STOW PLATE HINGES (3) REPLACED IAW CRJ 200 STM 51-42-06. (A)
PAX DOOR AFT SIDE PANEL STIFFENER (P/N 601R317745-7) CRACKED AT DOOR ASSIST MOTOR ASSY. STIFFENER (P/N 601R317745-7) REPLACED IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-13. (A)
CARGO DOOR SURROUND STRUCTURE, CHANNEL CRACKED AT FS 574 LBL 45 AND WL 79.5. CARGO DOOR SURROUND STRUCTURE CHANNEL AT FS 574 LBL 45 WL 79.5 REPLACED IAW CRJ 200 SRM 51-42-06. (A)
COCKPIT BULKHEAD FS 280 PUNCTURED AT LBL 34 AND WL 124. COCKPIT BULKHEAD FS 280 AT LBL 34 AND WL 124 REPAIRED IAW REO 601R-53-11-1414. (A)
BULKHEAD CLIPS CRACKED AT FS 280, LBL 9 AND WL 72. BULKHEAD CLIPS AT FS 280, LBL 9 AND WL 72 REPLACED IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-21. (A)
BULKHEAD CLIPS CRACKED AT FS 280, RBL 9 AND WL 72. BULKHEAD CLIPS AT FS 280, RBL 9 AND WL 72 REPLACED IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-21. (A)
PAX DOOR AFT DRAG ANGLE CRACKED. REPLACED ANGLE IAW SRM 51-42-06 AND 51-42-13. (A)
INTERCOSTAL CLIP AT FS 484, RBL 27, WL 72 IS CRACKED. INTERCOSTAL CLIP AT FS 484, RBL 27, WL 72 REMOVED IAW CRJ 200 SRM 51-42-06. NEW CLIP FABRICATED WITH S-6144-33 IAW CRJ 200 SRM 51-24-36 AND REPLACED IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-21. (A)
FUNCTIONAL TEST OF CREW ESCAPE HATCH FAIL CORROSION FOUND ON OUTER HANDLE SHAFT. OUTER HANDLE REPLACED. (A)
INTERCOSTAL AT FS 484 LBL 36, WL 72 IS CRACKED. NTERCOSTAL AT FS 484.0 LBL 36.0 REPAIRED IAW REO 601R-53-41-059. (A)
INTERCOSTAL CRACK ON LT SIDE AT STR 14 BTWN FRAME 621.00 AND 625.00. INTERCOSTAL REPLACED IAW SRM 51-42-06. (A)
NR 1 AND NR 2 HYDRAULIC SUPPORT BRACKETS CRACKED ON THE AFT LOWER EDGE. REPAIR PERFORMED ON NR 1 AND NR 2 HYDRAULIC MANIFOLD SUPPORT BRACKETS IAW CRJ 200 REO 601R-53-61-031 REV A. (A)
ON GEAR RETRACTION AFTER TAKEOFF, GEAR DISAGREE WARNING AND NLG DOOR OPEN WARNING, COMPLIED WITH QRH. IN ICING AFTER TAKEOFF FROM CONTAMINATED RUNWAY AT LESS THAN 200 KNOTS. VISUALLY CHECKED MLG AND NLG COMPONENTS, FOUND AND REMOVED ICE AND SNOW FROM NLG COMPONENTS AND SENSORS. PERFORMED LANDING GEAR EXTENSION AND RETRACTION IAW 32-30-00, OPS CHECK GOOD. (M)
BURNING RUBBER SMELL IN LAV. FOUND LAV EXHAUST FAN INOPERATIVE. REMOVED AND REPLACED LAV EXHAUST FAN IAW AMM 21-23-13. OPS CHECK GOOD. (M)
FLAPS FAIL CAUTION, FLAPS CONFIRMED AT ZERO DEGREES, COMPLIED WITH QRH. REMOVED AND REPLACED FLEX DRIVESHAFT NR 1, (PDU TO INBOARD FLAP) AS PER AMM 27-53-10, OPS TEST OF FLAPS GOOD AT THIS TIME. INSPECTED FLEX SHAFT, FOUND NO BARBER PULL. REMOVED MOISTURE AND LUBED REF AMM 27-53-10. (M)
AFTER TAKEOFF SELECTED GEAR UP, MAINS CAME UP AND STOWED FULLY. NLG REMAINED DOWN AND LOCKED. COMPLIED WITH QRH, NO HELP. INSPECTED NOSE GEAR, FOUND EXCESSIVE ICE ACCUMULATION, REMOVED ICE AS REQUIRED. PERFORMED SEVERAL GEAR SWINGS REF AMM 07-11-01. CLEANED PROXIMITY SWITCHES AS REQUIRED. NO DEFECTS NOTED. (M)
WITH BLEEDS SUPPLIED BY APU, STRONG FUEL ODOR NOTED. WITH BLEED SON ENGINE, NO ODOR NOTED. FOUND FUEL LEAKING FROM FCU ELBOW/NUT FITTING. REMOVED AND REPLACED O-RING. LEAK CHECK GOOD. NO FUEL SMELL NOTED. RED AMM 49-30-01. (M)
FOUND RIGHT SIDE FS 621 FLOOR SUPPORT ANGLE IS CRACKED APPROX .7 INCH LONG. MAINTENANCE CUT AWAY DAMAGE SECTION OF RIGHT 621 FLOOR SUPPORT ANGLE TRIMMED TO FIT P/N 601R53-61-117-2, 601R53-61-117-4, 601R53-61-117-6, AND DRILLED IAW REO 601R-53-61-117. (M)
FOUND LEFT SIDE FS 621 FLOOR SUPPORT ANGLE CRACKED APPROX .5 INCH LONG. MAINTENANCE CUT AWAY DAMAGED SECTION OF LEFT 621 FLOOR SUPPORT ANGLE, TRIMMED PARTS 601R-53-61-117-1 AND 601R53-61-117-3 TO FIT AND DRILLED IAW REO 601R-53-61-117. (M)
LEFT SIDE CARGO FLOOR SUPPORT EDGE MEMBER HAS MINOR SURFACE CORROSION IN AREA OF NUTPLATE FROM FS 574 TO FS 621. REMOVED CORROSION, TREATED, PRIMED AND PAINTED IAW CRJ SRM 51-21-06. (M)
RT MLG WHEEL WELL HYDRAULIC SWITCH BRACKET IS CRACKED ON INBOARD RADIUS. REMOVED CRACKED BRACKET AND INSTALLED A FABRICATED BRACKET FROM 2024 T-3 .050 INCH CLAD ALUMINUM IAW BSC STANDARD REPAIR 601R-53-0044E. (M)
LEFT MLG WHEEL WELL HYDRAULIC SWITCH BRACKET IS CRACKED IN OUTBOARD RADIUS. REMOVED CRACKED BRACKET AND INSTALLED A FABRICATED BRACKET FROM 2024 T3 .050 INCH CLAD ALUMINUM IAW BSC STANDARD REPAIR 601R-53-0044E. (M)
FOUND LEFT SIDE FS 484 INTERCOSTAL CRACKED AT LBL 36 APPROX .25 INCH LONG. REPAIRS ACCOMPLISHED IAW REO 601R-53-41-059A AND BSC STANDARD REPAIR 601R-53-0030A. (M)
PAX DOOR AFT DRAG ANGLE CRACKED APPROX .7 INCH LONG IN AREA OF DOOR ASSIST CABLE PULLEY BRACKET. REPAIRED PAX DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513. CUT AWAY DAMAGED AREA FABRICATED AND INSTALLED REPAIR ANGLE. (M)
AFTER TAKEOFF AT 300 FT, 160 KTS, RECEIVED GEAR UP DISAGREE NLG UPON SELECTION OF GEAR MLG UP AND LOCKED CAUTION WOW STATUS MESSAGE WOW OUTPUT FAILED FOLLOWED QRH DECLARED EMERGENCY LANDING UNEVENTFUL LANDING IN ORD. FOUND NOSE LANDING GEAR STRUT RETAIN COLLAR 90 OUT FROM WEAR DISARMED STRUT. INSPECTED FOUND LOWER RET ATN MISSING. REPLACED MINS AND RERACKED STRUT IAW 37-21-00 AND 32-21-15. NO DEFECTS NOTED. (M)
IDG NR 2 AMGER CAS MESSAGE AT TAKEOFF. TAKEOFF ABORTED AT 60 KNOTS. FOUND IDG LEAKING OIL FROM DRAIN PLUG FOUND DRAIN PLUG DAMAGED/ REMOVED AND REPLACED DRAIN PLUG IAW AMM 24-31-00. REMOVED AND REPLACED IDG NR 2. OPS AND LEAK CHECK GOOD.
BURNING ODOR AT APPROXIMATELY ISLE 7 NEAR OVERHEAD FLOURESCENT LIGHTING. IN PROGRESS.
AFTER TAKEOFF, RECEIVED EDP HYD. (M)