N918XJ
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| MESABA AVIATION INC | Operator | on 2008-04-24 | Operator named in NTSB report |
Accident & incident history
Operated by MESABA AVIATION INC (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
210 reports on file, 2009-06-02 – 2026-02-11.
Part: FITTING — CORRODED (NLG DOOR) · airframe 40,127 hrs · 28,253 cycles
CORROSION WAS FOUND ON FITTINGS LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). DUE TO EXCESSIVE CORROSION PER CRJ 900 SRM 51-10-06-001-001-A01 ON FITTINGS (4EAS) LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01
Part: FITTING — CORRODED (NLG DOOR) · airframe 40,127 hrs · 28,253 cycles
CORROSION WAS FOUND ON FITTINGS LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). DUE TO EXCESSIVE CORROSION PER CRJ 900 SRM 51-10-06-001-001-A01 ON FITTINGS (4EAS) LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01
Part: HINGE — CORRODED (NLG DOOR) · airframe 40,127 hrs · 28,253 cycles
CORROSION WAS FOUND ON FITTINGS LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE (4EAS). DUE TO EXCESSIVE CORROSION PER CRJ 900 SRM 51-10-06-001-001-A01 ON FITTINGS (4EAS) LH AND RH SIDE AT AFT NOSE LANDING GEAR DOOR AND ALSO ON FUSELAGE STRUCTURE WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 40,127 hrs · 28,253 cycles
CRACKED ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00. ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00 WERE REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 ,SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 40,127 hrs · 28,253 cycles
CRACKED ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00. ANGLES AT FLOOR SUPPORT STRUCTURE BTW FS 260.00 TO 280.00 AND RBL 12.00 AND LBL12.00 WERE REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 ,SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: WEB — CRACKED (ZONE 200) · airframe 40,127 hrs · 28,253 cycles
CRACK ON BIN SUPPORT MEMBRANE ON RBL34 AT FWD FACE OF MLG WHEEL WELL. BIN SUPPORT MEMBRANE ON RBL34 AT FWD FACE OF MLG WHEEL WELL WAS REPLACED PER CRJ900 SRM 51-41-02-001-001-A01
Part: STRIKER — CORRODED (ZONE 200) · airframe 40,127 hrs · 28,253 cycles
CORROSION ON STRIKER SILL AND ANGLE MOUNTING AT GALLEY SERVICE DOOR SURROUND STRUCTURE CORROSION ON STRIKER SILL AND ANGLE MOUNTING AT GALLEY SERVICE DOOR SURROUND STRUCTURE WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01, ANGLE MOUNTING WAS EVALUATED WHITIN LIMITS AND STRIKER SILL WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-23-101-002-A02, THEREFORE STRIKER SILL WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01
Part: SUPPORT — CORRODED (ZONE 100) · airframe 40,127 hrs · 28,253 cycles
CORROSION ON SETTLEMENT AREA OF BODY FAIRING ACCESS PANELS 195AB, 195BB, 196AR AND 195AL AT AFT BODY FAIRING SUPPORT STRUCTURE. CORROSION ON SETTLEMENT AREA OF BODY FAIRING ACCESS PANELS 195AB, 195BB, AND 195AL WAS REMOVED AND EVALUATED WITHIN LIMITS CRJ900 SRM 51-21-06-001-001-A01, CRJ-900 SRM 53-82-55-101-002-A02 AND ACCESS PANELS 196AR WAS REPLACED PER CRJ 900 SRM 51-23-00-001-001-A01 AT AFT BODY FAIRING SUPPORT STRUCTURE
Part: HINGE BRACKET — CORRODED · airframe 40,127 hrs · 28,253 cycles
CORROSION ON FWD HINGE AT FLAP STEP PLATE WAS FOUND. CORROSION ON FWD HINGE AT FLAP STEP PLATE WAS FOUND WAS EVALUATED OUT OFF LIMITS PER CRJ 900 SRM 51-10-06-001-001-A01 AND FWD HINGE AT FLAP STEP WAS REPAIRED PER EA NO:CRJ953-21661 REV.IR
Part: ANGLE — CRACKED (ZONE 300) · airframe 40,127 hrs · 28,253 cycles
CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER CRJ 900 SRM 55-31-00-201-001-A01
Part: ANGLE — CRACKED (ZONE 300) · airframe 40,127 hrs · 28,253 cycles
CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACKS ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WERE REPAIRED PER CRJ/900 SRM 55-31-00-201-001-A01
Part: ANGLE — CORRODED (ZONE 200) · airframe 40,127 hrs · 28,253 cycles
CORROSION ON FWD, AFT AND MID CAP ANGLE AT PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON FWD, AFT WAS REMOVED AND EVALUATED WITHIN LIMITS CRJ 900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-A01, AND MID CAP ANGLE AT PASSENGER DOOR SURROUND STRUCTURE WAS EVALUATED DUE TUE EXCESSIVED DAMAGE, THEREFORE WAS REPLACED PER CRJ900 SRM 51-41-02-001-001-A01
Part: COVER — CRACKED (ZONE 800) · airframe 40,127 hrs · 28,253 cycles
CRACKED HANDLE COVER AT PASSENGER DOOR. HANDLE COVER AT PASSENGER DOOR WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01
Part: WEB — CRACKED (ZONE 100) · airframe 40,127 hrs · 28,253 cycles
CRACKED FLOOR WEB LEFT SIDE AT_ ELECTRICAL BAY (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00. FLOOR WEB LEFT SIDE AT_ ELECTRICAL BAY (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ 900 SRM 53-11-43-201-001-A01
Part: SKIN — CRACKED (THRUST REVERSER) · airframe 40,127 hrs · 28,253 cycles
TORN UPPER AND LOWER AFT SEAL AT RT UPPER AND LOWER THRUST REVERSE ALSO CRACK AFT SEAL PLATE AT RT LOWER THRUST REVERSE. CRACK AFT SEAL PLATE AT RT LOWER THRUST REVERSE WAS REPAIRED PER EA CRJ954-21516 REV IR AND UPPER AND LOWER AFT SEAL AT RT UPPER AND LOWER THRUST REVERSE WERE REPLACED IAW SRM 51-42-10-001-001-A01 AND SRM 51-42-13-001-001-A01.
Part: SUPPORT — CRACKED (ZONE 100) · airframe 40,127 hrs · 28,253 cycles
CRACK AT CORNERS OF SUPPORT AT THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT SUPPORT AT THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
Part: FITTING — CORRODED (ZONE 200) · airframe 40,127 hrs · 28,253 cycles
CORROSION ON FITTING (10 EACH) BTW FS280/FS379 AND LBL42/RBL42 AT FLOOR STRUCTURE. CORROSION ON FITTING (10 EAÿ½S) BTW FS280/FS379 AND LBL42/RBL42 AT FLOOR STRUCTURE WAS CLEANED, REMOVED, EVALUATED WHITIN LIMITS, EVALUATED DUE TO EXCESSIVE DAMAGE AND REPLACED PER CRJ900 SRM 51-26-00-001-001-A01, PER CRJ-900 SRM 51-21-06-001-001-401, CRJ 900 SRM 53-00-01-101-001-A01, CRJ 900 SRM 53-21-43-101-001-A03 AND CRJ900 SRM 51-42-21-001-001-A01
Part: FAIRING — CRACKED (THRUST REVERSER) · airframe 40,127 hrs · 28,253 cycles
CRACKED THRUST-REVERSER AFT UPPER HINGE LINE FAIRING 443BT ALSO BEND AND WEAR AFT LOWER HINGE LINE FAIRING 443BB AT RH ENGINE. THRUST-REVERSER AFT UPPER HINGE LINE FAIRING 443BT WAS REPLACED PER CRJ900 AMM 54-12-01 AND AFT LOWER HINGE LINE FAIRING 443BB AT RH ENGINE WAS CLEAN AND CONFORMED, THEREFORE NO WEAR AND CRACKS WERE FOUND PER CRJ 900 SRM 51-24-21-001-001-A01 AND CRJ900 SRM 51-26-00-001-001-A01
Part: WEB — CRACKED (ZONE 100) · airframe 40,127 hrs · 28,253 cycles
CRACKED FLOOR WEB RIGHT SIDE AT_ ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS193.00 CRACKED DOUBLER AT FLOOR WEB RIGHT SIDE AT_ ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPLACED PER CRJ-900 SRM 53-11-43-201-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: FITTING — CORRODED (ZONE 200) · airframe 40,127 hrs · 28,253 cycles
CORROSION ON PROXIMITY SENSOR PX36 AT GALLEY SERVICE DOOR CORROSION ON FITTING ASSY, SLIDE AT GALLEY SERVICE DOOR WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND DUE TO EXCESSIVE DAMAGE WILL BE REPLACE PER CRJ 900 SRM 53-21-43-101-001-A03 AND WAS REPLACED PER CRJ-900 AMM 53-21-23, OPERATIONAL TEST SATISFACTORY
Part: HINGE — CORRODED (ACCESS DOOR) · airframe 40,127 hrs · 28,253 cycles
CORROSION ON HINGE(2EAS), HINGE ARMS(2EAS) AND HARDWARE ATTACHED TO ACCESS DOOR 196DR HINGE ASSY LWR P/N CC670-39189-1 WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND CORROSION WAS NOT FOUND AND DUE TO EXCESSIVE CORROSION ON HINGES OUTBD (NP: CC670-39095-1), INBD (NP: CC670-39096-1) AND HINGE UPPER (P/N: CC670-39109-5) WERE REPLACED PER CRJ/900 SRM 53-61-43-101-001-A02, SRM 51-10-06-001-001-A01 AND SRM 51-41-02-001-001-A01
Part: HINGE — CORRODED (ACCESS DOOR) · airframe 40,127 hrs · 28,253 cycles
CORROSION ON HINGE(2EAS), HINGE ARMS(2EAS) AND HARDWARE ATTACHED TO ACCESS DOOR 196DR HINGE ASSY LWR P/N CC670-39189-1 WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND CORROSION WAS NOT FOUND AND DUE TO EXCESSIVE CORROSION ON HINGES OUTBD (NP: CC670-39095-1), INBD (NP: CC670-39096-1) AND HINGE UPPER (P/N: CC670-39109-5) WERE REPLACED PER CRJ/900 SRM 53-61-43-101-001-A02, SRM 51-10-06-001-001-A01 AND SRM 51-41-02-001-001-A01
Part: HINGE — CORRODED (ZONE 100) · airframe 40,127 hrs · 28,253 cycles
CORROSION ON HINGE(2EAS), HINGE ARMS(2EAS) AND HARDWARE ATTACHED TO ACCESS DOOR 196DR HINGE ASSY LWR P/N CC670-39189-1 WAS CLEANED PER CRJ900 SRM 51-26-00-001-001-A01 AND CORROSION WAS NOT FOUND AND DUE TO EXCESSIVE CORROSION ON HINGES OUTBD (NP: CC670-39095-1), INBD (NP: CC670-39096-1) AND HINGE UPPER (P/N: CC670-39109-5) WERE REPLACED PER CRJ/900 SRM 53-61-43-101-001-A02, SRM 51-10-06-001-001-A01 AND SRM 51-41-02-001-001-A01
Part: LANDING — CRACKED (ZONE 800) · airframe 40,127 hrs · 28,253 cycles
CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS MANUFACTURED PER EA NO: CRJ953-21561 REV IR, DWG CC670-33151-6 REV ""D"", AND REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01.
Part: SUPPORT — CRACKED (ZONE 100) · airframe 40,127 hrs · 28,253 cycles
CRACKED INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE WAS REPLACED PER CRJ900 SRM 51-41-10-001-001-A01 AND SRM 51-42-06-001-001-A01
Part: LANDING — CRACKED (ZONE 800) · airframe 40,127 hrs · 28,253 cycles
"CRACK ON AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS MANUFACTURED PER EA NO: CRJ953-21561 REV IR, DWG CC670-33151-6 REV ""D"", AND REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01."
Earlier reports · 2009–2023 · 184 reports
2023
Part: POST — CRACKED (UNKNOWN) · airframe 34,743 hrs · 24,155 cycles
UPON REMOVAL LBL 27 POST WAS FOUND TO BE CRACKED. INSTALLED SERVICABLE LBL 27 POST IAW SERVICE BULLETIN FIGURE 105, SHEET 4 OF 8.
2022
Part: FITTING — CRACKED · airframe 32,903 hrs · 22,706 cycles
RH FWD EMERGENCY EXIT DOOR HAS CRACK IN AFT PROX SENSOR FITTING. REPAIRED CRACKED STRUCTURE IN RH FWD EMERGENCY EXIT DOOR PER EA CRJ952-14082 REV IR, DATED 7/7/2022
Part: SKIN PANEL — CORRODED · airframe 32,903 hrs · 22,706 cycles
PASSENGER DOOR INNER SKIN CORRODED. REPLACED PASSENGER DOOR INNER SKIN.
Part: CHANNEL — CHAFED · airframe 32,903 hrs · 22,706 cycles
RH LOWER TRANSCOWL LATCH DOOR COAMING CHANNEL CHAFED. REPLACED CHANNEL.
Part: PANEL — CORRODED · airframe 32,903 hrs · 22,706 cycles
PASSENGER DOOR TOP PANEL AT UPPER STAIR WEB CORRODED. REPLACE PAX DOOR TOP PANEL AT UPPER STAIR WEB.
Part: BRACKET — CRACKED · airframe 32,903 hrs · 22,706 cycles
LH UPPER TRANSCOWL OUTBOARD-FWD STANDOFF ("A" BRACKET) CRACKED/BROKEN. REPLACED LH UPPER TRANSCOWL OUTBOARD-FWD STANDOFF.
Part: BRACKET — CRACKED · airframe 32,903 hrs · 22,706 cycles
LH UPPER TRANSCOWL INBOARD-FWD STANDOFF ("A" BRACKET) CRACKED/BROKEN. REPLACED LH UPPER TRANSCOWL INBOARD-FWD STANDOFF..
Part: TRANSCOWL — CRACKED · airframe 32,903 hrs · 22,706 cycles
AFTER REMOVAL OF Z-ANGLE ON UPPER RH TRANSCOWL (FOR REPAIR OF DAMAGED FASTENERS) FOUND 1.159" CRACK IN INNER PERFORATED SKIN. REPAIRED RH UPPER TRANSCOWL SKIN PER EA CRJ954-13905 REV B.
Part: SILL DRAIN — CORRODED · airframe 32,903 hrs · 22,706 cycles
FLOOR SILL CORRODED AT FS 565.00 LH SIDE INSTALLED NEW LH LOWER FLOOR SILL FROM FS517 TO FS565 REF CRJ900 SRM 51-42-06-001-001-A01
Part: FRAME — CORRODED · airframe 32,903 hrs · 22,706 cycles
FRAME INTERNAL TO PAX DOOR AT FS313.56 BETWEEN DD4-DD5 HAS INTERGRANULAR CORROSION AROUND RIVET HOLES. REMOVED AND REPLACED CORRODED FRAME WITH NEW REPLACEMENT FRAME (P/N 601R318086-1) AND CLEAT (P/N 600-31902-269) USING ALL NEW HARDWARE. REF BOMBARDIER DWG 601R31702 REV-N AND CRJ 900 SRM 51-42-06-001-001-A01. ALL CHECKS GOOD.
Part: LATCH — CHAFED · airframe 32,903 hrs · 22,706 cycles
RH UPPER TRANSCOWL LATCH DOOR CHAFED IN MULTIPLE AREAS REPLACED RH UPPER TRANSCOWL LATCH DOOR
Part: FLOOR PANEL — CORRODED · airframe 32,903 hrs · 22,706 cycles
BACKUP SILL, STRINGER 21L, FS310-333 CORRODED BER. REPLACED BACKUP SILL, STRINGER 21L, FS310-333.
Part: PANEL — CORRODED · airframe 32,903 hrs · 22,706 cycles
PASSENGER DOOR, TOP PANEL ON STAIR WEB, AROUND SCREW HOLES HAS EVIDENCE OF CORROSION. REPLACED PASSENGER DOOR TOP PANEL ON STAIR WEB
Part: CHANNEL — CHAFED · airframe 32,903 hrs · 22,706 cycles
RH LOWER TRANSCOWL CHANNEL C, FORWARD, IS CHAFED REPLACED CHANNEL C, FORWARD
Part: LATCH — CHAFED · airframe 32,903 hrs · 22,706 cycles
LATCH DOOR COAMING CHAFED ON RH LOWER TRANSCOWL. " REPLACED LATCH DOOR COAMING ON RH LOWER TRANSCOWL."
Part: TRACK — CORRODED · airframe 32,903 hrs · 22,706 cycles
SEAT TRACK AT RBL9, FS349-379 IS CORRODED IN SEVERAL AREAS, ON SEVERAL ELEMENTS. REPLACED SEAT TRACK PN SH670-32159-1 WITH NEW PART.
Part: INTERCOSTAL — CORRODED (PASSENGER DOOR) · airframe 32,903 hrs · 22,706 cycles
PASSENGER DOOR INTERNAL STRUCTURE AT MID INTERCOSTAL DD6 HAS EVIDENCE OF CORROSION. REPLACED MID INTERCOSTAL DD6 PER CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-01-001-001-A01, DWG 601R31702 REV N.
Part: FRAME — CORRODED (FRAME 23-24L) · airframe 32,903 hrs · 22,706 cycles
FS1031.00 FRAME HAS CORROSION ON ITS ATTACHED FLANGE BETWEEN STGR23L AND 24L
Part: PANEL — CHAFED (LH INBD FLAP) · airframe 32,903 hrs · 22,706 cycles
LH INBOARD FLAP LEADING EDGE SKIN PANEL 584GB IS CHAFED FROM CONTACT WITH MOVABLE FLAP VANE. REPLACED PANEL 584GB WITH NEW SKIN PANEL PN CC670-14178-1.
2020
Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 29,002 hrs · 19,398 cycles
AWR: DELAMINATED FLOOR PANELS NBR , NRB 281DLF AND 282JRF AT AFT CARGO COMPARTMENT (COMPOSITE). SUMMARY: FLOOR PANELS NBR , NRB 281DLF AND 282JRF AT AFT CARGO COMPARTMENT WERE REPLACED PER CRJ-900 AMM 53-00-47-400-803 (CONFIG A03)
2019
Part: UNKNOWN — NONE (NONE) · airframe 28,444 hrs · 18,982 cycles
WHILE INCORPORATING SB607BA-57-020, CLEARANCE ISSUES WITH 1 FASTENER EACH SIDE UNDER FITTING. COMPLIED WITH BOMBARDIER REO 690-57-21-322 REV. DATED 2019-11-08. WVAC EMP STAMP 771.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,040 hrs · 18,659 cycles
ESCAPE PATH LIGHTS IN GALLEY (R & L) BULBS INOP PN OL3071BPEGPL. REPLACED INOP BULBS IAW AMM 33-51-11. OP CK GOOD PN OL3071BPEGPL.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 26,657 hrs · 17,623 cycles
OUT OF LIMITS CORROSION ON STRINGER SPLICE 25R IN STA FS= 329 TO FS= 339 AT MAIN AVIONICS COMPARTMENT. STRINGER SPLICE 25R BTW FS329/339 WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR 6D AND SRM 51-42-20-001-001-A0 1 PAR 6E.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 26,657 hrs · 17,623 cycles
CORROSION ON STRINGER 25R IN STA FS= 280 TO FS= 329 AT MAIN AVIONICS COMPARTMENT. CORROSION LEVEL 2; STRINGER 25R IN STA FS= 280 TO FS= 329 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01.
Part: STRIKER — CORRODED (FUSELAGE) · airframe 26,657 hrs · 17,623 cycles
CORROSION ON LOWER STRIKER IN STA FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. LEVEL CORROSION 2. LOWER STRIKER IN STA FS= 319 TO FS= 349 AND 44RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR 6 C.
Part: ANGLE — CRACKED (PAX DOOR) · airframe 26,657 hrs · 17,623 cycles
CRACK IN AFT SIDE PANEL LOWER ANGLE AT PASSENGER DOOR. AFT SIDE PANEL LOWER ANGLE AT PASSENGER DOOR WAS REPAIRED PER SRM 52-11-04-201-A01.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,657 hrs · 17,623 cycles
CORROSION ON FLOORBEAM IN STA FS= 280 BETWEEN 11 RBL TO 12RBL AT PAX CABIN FWD WET AREA. FLOORBEAM IN STA FS= 280 BETWEEN 11RBL TO 12RBL AT PAX CABIN FWD WET AREA. WAS REPLACED PER SRM 51-42-06-001-00 1-A01 PAR 6 C; SRM 51-42-20-001-001-A01 PAR 6 C AND SRM 51-42-13-001-001-A01 PAR 6 C.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 26,657 hrs · 17,623 cycles
CORROSION ON SUPPORT MOUNTING ANGLE IN STA FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. LEVEL CORROSION 2. SUPPORT MOUNTING ANGLE IN STA FS= 319 TO FS= 349 AND 41RBL AT GALLEY SERVICE DOOR LOWER SILL, FWD WET A REA. WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR 6.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 26,657 hrs · 17,623 cycles
CRACK ON FLOORBEAM UPPER/AFT FLANGE IN STA FS= 280 AND 14LBL AT PAX CABIN FWD WET AREA. FLOORBEAM WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR 6 C; SRM 51-42-20-001-001-A01 PAR 6 C. AND SRM 5 1-42-13-001-001-A01 PAR 6 C
Part: FRAME — CORRODED (FUSELAGE) · airframe 26,657 hrs · 17,623 cycles
CORROSION ON FRAME IN STA FS= 349 BTW STR 26R TO 27 AT MAIN AVIONIC S COMPARTMENT. LEVEL CORROSION 2. FRAME IN STA FS= 349 BTW STR 26R TO 27 AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER REO 670-53-21-1 281.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,657 hrs · 17,623 cycles
CORROSION ON FLOOR SEAT RAIL IN SECTIONS FS= 375 TO FS= 485, 9LBL AT PAX CABIN FWD WET AREA. FLOOR SEAT RAILS IN SECTIONS FS= 375 TO FS= 485, 9LBL AT PAX CABIN FWD, WAS REPLACED PER SRM 53-21-49-101-001 -A01 AND AMM 53-00-49-400-801-A7.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 26,657 hrs · 17,623 cycles
CORROSION ON FWD PRESSURE SILL, WINGBOX, LT SIDE, IN STA FS= 748 TO FS= 750 BETWEEN 36LBL TO 42LBL AT PAX CABIN. LEVEL CORROSION 1. CORROSION WAS REMOVED PER SRM 51-21-06-001-001-A01 AND FLAPPEEN WAS PERFORMED ON REPAIRED AREA PER SRM 51-24-11-001-001-A01 IN REFERENCE TO REO 690-53-41-171 REV-, STEP 3.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 26,657 hrs · 17,623 cycles
CORROSION ON MID/AFT PRESSURE SILL AND SILL-SPLICE, WINGBOX, RT SIDE, IN STA FS= 792 TO FS= 802 BETWEEN 36RBL TO 42RB L AT PAX CABIN. LEVEL CORROSION 1. CORROSION WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND FLAPPEEN WAS PERFORMED ON REPAIRED AREA PER SRM 51-24-11-001-001-A01 IN REFERENCE TO REO 690-53-41-171 REV-, STEP 3.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 26,657 hrs · 17,623 cycles
CORROSION ON MID/AFT PRESSURE SILL AND SILL-SPLICE, WINGBOX, LT SIDE, IN STA FS= 792 TO FS= 802 BETWEEN 36LBL TO 42LB L AT PAX CABIN. LEVEL CORROSION 1. CORROSION WAS REMOVED PER SRM 51-21-06-001-001-A01 AND FLAP PEEN WAS PERFORMED ON REPAIRED AREA PER SRM 51-24-11-001-001-A01 IN REFERENCE TO REO 690-53-41-171 REV-, STEP 3.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 26,657 hrs · 17,623 cycles
INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 485 TO FS= 572, STGR 15LH/RH ] [ FS= 572 TO FS= 661+16, STGR 15LH/RH ] [ FS= 661+16 TO FS= 677, STGR 15LH ] [FS= 661+16 TO FS= 661+90, STGR 15 RH ] [FS= 661+90 TO FS= 677, STGR 15RH ] AT PAX CABIN. (CPAX) (TCI: 5 3-20-217). COMPLETE: SUMMARY. SEAT RAILS IN SECTIONS [ FS= 485 TO FS= 572, STGR 1 5LH/RH ] [ FS= 572 TO FS= 661+16, STGR 15LH/RH ] [ FS= 661+16 TO FS= 677, STGR 15LH ] [ FS= 661+16 TO FS= 661+90, STGR 15RH ] [ FS= 661+90 TO FS= 677, STGR 15RH ] AT PAX CABIN WERE REPLACED PER CRJ900 AMM 53-00 -49-400-801-A7.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,657 hrs · 17,623 cycles
CORROSION ON FLOORBEAM LBL27 STA FS=1032 AT AFT CARGO COMPARTMENT. FLOORBEAM LBL27 STA FS=1032 AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 51-42-21-001-001-A01 AND 51-00-41-201-001-A03 AND CRJ-953-08282.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 26,657 hrs · 17,623 cycles
INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS IN SECTIONS [FS= 693 TO FS= 830, 9LBL/9RBL ] [FS= 830 TO FS=849, 9LBL/9RBL ] [FS= 849 TO 977, 9LBL/9RBL ] AT PAX CABIN. (CPAX) (TCI: 100-20). COMPLETE: SUMMARY. FLOOR SEAT RAILS IN SECTIONS [ FS= 693 TO FS= 830, 9LBL/9RBL ] [ FS= 830 TO FS= 849, 9LBL/9RBL ] [ FS= 849 TO 977, 9LBL/9 RBL ] AT PAX CABIN WERE REPLACED PER CRJ900 AMM 53-00-49-400-801-A07 .
Part: CANISTER — CRACKED (RT WING) · airframe 26,657 hrs · 17,623 cycles
INITIAL INSPECTION: CRACK IN CANISTER, WELDED NR 3 IN STA WS148 AT RT MAIN FUEL TANK. CANISTER WELDED NR 3 IN STA WS148 AT RT MAIN FUEL TANK. WAS REPAIRED PER REO 670-57-42-577 REV.
Part: CANISTER — CRACKED (LT WING) · airframe 26,657 hrs · 17,623 cycles
INITIAL INSPECTION: CRACK IN CANISTER, WELDED NR 3 IN STA WS148 AT LT MAIN FUEL TANK. CANISTER WELDED NR 3 IN STA WS148 AT LT MAIN FUEL TANK. WAS REPAIRED PER REO 670-57-42-577 REV.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 26,657 hrs · 17,623 cycles
INITIAL INSPECTION: CORROSION ON SIDE SEAT RAILS IN SECTIONS [ FS= 677 TO FS= 720, STGR 15LH/RH ] [FS= 744 TO FS= 761, STGR 15LH/RH ] [ FS= 785 TO 847+16, STGR 15LH/RH ] [ FS= 847+16 TO FS= 906, STGR 15LH ][FS= 847+16 TO FS= 865, STGR 15RH ] AT PAX CABIN. (CPAX) (TCI: 53-20-23. COMPLETE: SUMMARY. SIDE SEAT RAILS IN SECTIONS [ FS= 677 TO FS= 720, STGR 15LH/RH ] [ FS= 744 TO FS= 761, STGR 15LH/RH ] [ FS= 785 TO 847+16, STGR 15LH/RH ] [ FS= 847+16 TO FS= 906, STGR 15LH ] [ FS= 847+16 TO FS= 865, STGR 15RH ] AT PAX CABIN WERE REPLACED PER CRJ900 AMM 53-00-4.
2018
Part: FLAP — PUNCTURED (RT WING) · airframe 26,657 hrs · 17,623 cycles
PUNCTURE AT RIGHT-WING INBOARD FLAP ON FLS33. AREA WAS REPAIRED PER PER SRM 57-52-01-201-001-A01 PAR 4 D (ET)(HFEC) WAS ACCOMPLISHED, PER SRM 57-52-01-201-001-A01 PAR 4 & NDT PART 01, 51-20-006-250. NO CRACKS WERE FOUND AFTER TRIM OUT.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 26,657 hrs · 17,623 cycles
CORROSION ON INTERCOSTAL BTW STA FS310 TO FS319 AT STR 20R BELOW FLOOR STRUCTURE. LEVEL CORROSION 2. INTERCOSTAL BTW STA FS310 TO FS319 AT STR 20R BELOW FLOOR STRUCTURE WAS REPLACED PER SRM 51-42-21-001-001-A01.
Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 24,989 hrs · 16,407 cycles
RIGHT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-15, OPS CHECKED GOOD.
Part: LIGHT — MISSING (MAIN CABIN) · airframe 24,895 hrs · 16,344 cycles
FA REPORTED A PORTION OF THE EMERGENCY LIGHT STRIP IS MISSING SEAT 13A/B. LOCATED AND REINSTALLED THE EMERGENCY LIGHT STRIP IWA AMM 33-51-19
2017
Part: UNKNOWN — ODOR (CABIN) · airframe 23,882 hrs · 15,627 cycles
FA REPORTED FUMES IN CABIN. EMERGENCY PROCEDURES COMPLETE. EMERGENCY DECLARED. COMPLIED WITH TS 002737. RAN BOTH ENGINES ALONG WITH APU IAW AMM 71-00-00. OPERATED PACKS FULL COLD AND FULL HOT AND NO NOTICEABLE ODOR. ALSO SWITCHED BLEED SOURCES TO ISOLATE ENGINES AND TESTED PACKS, NO ODOR NOTED. OK FOR SERVICE.
Part: SEAL — BROKEN (PBE) · airframe 23,397 hrs · 15,279 cycles
FORWARD PBE IN WARDROBE HAS BOTH SEALS BROKEN. REPLACED THE SEALS IAW AMM 35-31-06.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 23,343 hrs · 15,239 cycles
FORWARD EMER FLASHLIGHT AT FLT ATTENDANT STA IS NOT SECURED OR CHARGED. REMOVED AND REPLACED FLASHLIGHT BATTERY AND RESECURED IAW AMM 25-61-00.
Part: CONNECTOR — DEFECTIVE (BLEED AIR SYS)
THRU 17,000 FT ON CLIMB OUT BOTH PACKS FAILED, AIRCRAFT DEPRESSURIZED. WE LEVELED THEN DESCENDED TO 10,000. WE COMPLETED THE QRH AND RETURNED TO CVG. DUE TO ANTI-ICE LEAK DETECTION CONTROLLER (AILC) DETECTING A BLEED LEAK IN BOTH A AND B SYSTEMS. THE BLEED AIR SOURCE WAS AUTOMATICALLY SHUTOFF WHICH STOPPED AIRFLOW TO BOTH PACKS. BOTH BLEED LEAK INDICATING SYSTEMS AND BLEED DUCTING HAVE BEEN ADDRESSED, SEE AML'S FOR DETAILS. BOTH PACKS OPERATE NORMAL, SEE AML FOR DETAILS. A/C OK FOR SERVICE. FOUND LEFT BLEED LOOP B WITH HI RESISTANCE USED FREEZE SPRAY AND TAPPED ON CONNECTORS MT 138 P1 AND P2 MT203 P1, MT226 P2, MT142 P1 AND P2 FOUND 90 DEG CONNECTOR AT MT138 P1 WITH FLUCTUATION WHEN TAPPED. REMOVED AND REPLACED 90 DEG CONNECTOR MT138 P1 IAW AMM 36-21-00. LT BLEED LOOP B FINAL RESISTANCE 47 OHMS AND STABLE USED FIM 36-21-01 FOR TROUBLESHOOTING. EMERGENCY WAS DECLARED, AIR-RETURNING BACK TO CVG.
Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 22,457 hrs · 14,593 cycles
PAX OXYGEN MASKS DEPLOYED OVER 18 C+D. REINSTALLED PAX OXYGEN MASK OVER 18 C+D PER AMM 35-21-09. "
Part: LIGHT — MISSING (CABIN) · airframe 22,269 hrs · 14,474 cycles
EMERGENCY LIGHT MISSING IN ROW 13 A/B. REINSTALLED REPLACED THE LIGHT IAW AMM 33-51-01.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 22,191 hrs · 14,414 cycles
FO'S EMERGENCY FLASH LIGHT INOP. REMOVED AND REPLACED FO'S EMERGENCY FLASHLIGHT AND BRACKET IAW AMM 25-61-02. NO FURTHER DEFECTS NOTED.
2016
Part: PIN — NOT SEATED (CABIN) · airframe 22,086 hrs · 14,341 cycles
LT FWD OVERWING EMERG EXIT LOWER EMERG LIGHT EXIT SIGN INOP. FOUND PIN BUSHED/NOT LOCKED AT CONNECTOR J5422. SEATED/LOCKED PIN IAW ESPM 20-26-00. EMER LIGHT OPS TEST GOOD IAW AMM 33-51-00-710-802-A16.
Part: FITTING — CHAFED (RT WING) · airframe 22,086 hrs · 14,341 cycles
RT WING AFT BOTTOM INBD LUG ON WING ATTACHMENT FITTING IS CHAFED. REPAIRED IAW REO 690-57-11-069 REV-- DATED 12/28/16.
Part: HINGE — GOUGED (FUSELAGE) · airframe 22,086 hrs · 14,341 cycles
AFT LUG LANDING FOR PAX DOOR PIANO HINGE ON FUSELAGE SIDE IS GOUGED FROM ROLL PIN. REPAIRED PAX DOOR AFT LUG LANDING FOR PAX DOOR PIANO HINGE ON FUSELAGE SIDE IAW REO:670-53-21-582 REPAIR TYPE 4.
Part: FITTING — CHAFED (WING) · airframe 22,086 hrs · 14,341 cycles
LT AFT BOTTOM INBD LUG ON WING ATTACHMENT FITTING IS CHAFED. REPAIRED IAW REO 690-57-11-069 REV--DATED 12/28/16.
Part: SUPPORT — CORRODED (BS 265-280) · airframe 22,086 hrs · 14,341 cycles
CORROSION ON FWD JACKING FITTING AND LT JACK FITTING SUPPORT. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND EA CRJ953-05156.
Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 22,086 hrs · 14,341 cycles
RIGHT FLOOR SUPPORT IS CORRODED FROM BS 280.00 - 319.70. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01.
Part: PLATE — CHAFED (VERTICAL STAB) · airframe 22,086 hrs · 14,341 cycles
AFT FRAME CHAFED ON THE LT & RT SIDES. REMOVED AND REPLACED LT & RT PLATES ON VERT STAB AFT FRAME BULLET FAIRING IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-25-16-001-001-A01. P/N PLATE : AV670-21413-007 ; P/N PLATE : AV670-21413-008
Part: DOOR SILL — CORRODED (BS 1000) · airframe 22,086 hrs · 14,341 cycles
FOUND CORROSION ON AFT CARGO DOOR SILL AROUND NUTPLATE HOLE JUST AFT OF BS 1000. REMOVED AND REPLACED THE AFT CARGO DOOR SILL IAW SRM 51-42-06-001-001-A01, AND 51-42-13-001-001-A01.
Part: SKIN — CHAFED (RUDDER) · airframe 22,086 hrs · 14,341 cycles
RUDDER RT LOWER L/E SKIN IS CHAFED APPROX 36"L X .3"W X .005"D. REMOVED AND REPLACED L/E SKIN IAW SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-25-01-001-001-A01.
Part: STRINGER — CRACKED (FUSELAGE) · airframe 22,086 hrs · 14,341 cycles
FS 280 AFT OF BULKHEAD, STRINGER 3L IS CRACKED. REPAIRED FS 280 AFT OF BULKHEAD STRINGER 3L IAW EOR53568.
Part: PANEL — CHAFED (RT WING) · airframe 22,086 hrs · 14,341 cycles
RIGHT WING PANEL 699AB HAS CHAFE. LOCATED AND DRILLED A NEW PANEL IAW SRM 51-40-11-001-001-A01.
Part: PANEL — CHAFED (RT WING TE FLAP) · airframe 22,086 hrs · 14,341 cycles
RIGHT FLAP VANE L/E PANEL 684ET HAS TWO MINOR CHAFES. REMOVED & REPLACED THE PANEL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, & 51-25-01-001-001-A01.
Part: PANEL — CHAFED (RT WING TE FLAP) · airframe 22,086 hrs · 14,341 cycles
RIGHT FLAP VANE L/E PANEL 684HT HAS A MINOR CHAFE. REMOVED & REPLACED THE PANEL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, & 51-25-01-001-001-A01.
Part: HINGE — CORRODED (PAX DOOR) · airframe 22,086 hrs · 14,341 cycles
PAX DOOR TOP STEP LOWER HINGE CRACKED / MISSING LUG. REMOVED & REPLACED LOWER HINGE TO PAX DOOR TOP STEP IAW SRM 51-40-11-001-001-A01 & SRM 51-42-06-001-001-A01.
Part: HINGE — BENT (CARGO BAY) · airframe 22,086 hrs · 14,341 cycles
AFT BAGGAGE BAY STEP PLATE AFT HINGE IS BENT AND BINDING. REMOVED TAPE. REMOVED AND REPLACED HINGE AT AFT BAGGAGE BAY STEP PLATE AFT HINGE IAW SRM 51-40-11-001-001-A01 AND SRM 51-42-06-001-001-A01.
Part: POST — CORRODED · airframe 22,086 hrs · 14,341 cycles
LEFT BS 280 FLIGHT DECK DOOR POST IS CORRODED ON LOWER END. REPAIRED IAW CRJ953-05137 REV A.
Part: ATTACH ANGLE — CORRODED (PAX DOOR) · airframe 22,086 hrs · 14,341 cycles
PAX DOOR BOTTOM STEP LOWER ATTACHMENT ANGLE HAS ELONGATED FASTENER HOLE. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE ANGLE, BOTTOM "C" P/N:601R-317726-3 IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: FITTING — CORRODED (PAX DOOR) · airframe 22,086 hrs · 14,341 cycles
FWD CLOSING FITTING AT PASSENGER DOOR OPENING IS CORRODED. LOCATED, DRILLED AND INSTALLED A NEW FITTING IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
Part: ANGLE — CORRODED (BS 310-349) · airframe 22,086 hrs · 14,341 cycles
PAX DOOR KICK PLATE IS CORRODED. REMOVED AND REPLACED THE KICK PLATE IAW SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,707 hrs · 14,069 cycles
LIGHTING STRIPS FORWARD CABIN. R&R FORWARD CABIN EMERGENCY FLOOR TRACK LIGHT IAW AMM 33-51-01.
Part: LIGHT — UNSECURE (CABIN) · airframe 21,405 hrs · 13,838 cycles
EMERGENCY FLOOR STRIP AT EXIT ROW FELL OFF. REINSTALLED EMERGENCY FLOOR PATH MARKING STRIP, EXIT ROW 15 A AND B IAW AMM 33-51-01. NO FURTHER DETAILS NOTED.
Part: OXYGEN MASK — DAMAGED (COCKPIT) · airframe 21,396 hrs · 13,832 cycles
CAPTAIN SIDE, O2 MASK BUTTON USED TO PURGE MASK MISSING PLASTIC BUTTON PIECE. R & R CREW O2 MASK IAW AMM 35-11-12. PERFORMED OPS TEST OF CREW O2 SYS. OPS TEST GOOD. CREW O2, 1790 PSI IAW AMM 23-51-00 AND AMM 35-10-00.
Part: LIGHT — MISSING (CABIN) · airframe 21,380 hrs · 13,819 cycles
LIGHT STRIP NEXT TO FORWARD LAV AND BY EXIT ROWS 12+13 MISSING. REINSTALLED FLOOR STRIPS ON FWD LAV AND ROWS 12+13. NO FURTHER DEFECTS NOTED. REINSTALLED AS REQUIRED.
Part: LIGHT — MISSING (ROW 12C) · airframe 21,179 hrs · 13,680 cycles
EMERGENCY LIGHT MISSING BY ROW 12C. SECURED THE LIGHT.
Part: LIGHT — UNSECURE (GALLEY) · airframe 21,119 hrs · 13,639 cycles
EMERGENCY LIGHT IN GALLEY NEEDS TO BE SECURED. INSTALLED THE EMERGENCY LIGHT IAW AMM 25-25-00. OK FOR SERVICE.
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 20,744 hrs · 13,383 cycles
PILOT SIDE FLASHLIGHT FLASHING LIGHT NOT FLASHING. R & R PILOT SIDE FLASHLIGHT IAW AMM 25-61-02. OPERATIONS CHECKED GOOD.
Part: GLOWSTRIP — UNSECURE (CABIN) · airframe 19,921 hrs · 12,837 cycles
LIGHTING STRIP IN FRONT OF PAX DOOR CAME UNGLUED. REATTACHED FLOOR GLOW STRIP IAW AMM 25-33-01. OK FOR SERVICE.
2015
Part: G SWITCH — INOPERATIVE (ELT) · airframe 19,396 hrs · 12,469 cycles
DURING OPERATIONS TEST OF ELT, FOUND G SWITCH DID NOT FUNCTION. R & R ELT IAW AMM 25-62-02-400-801. ELT RAMP TESTED GOOD.
Part: PLATE — CHAFED (LT COWLING) · airframe 18,699 hrs · 11,979 cycles
TASK CARD 900-71-430-100, LEFT ENG LOWER CORE COWL BLOW OUT DOOR HINGE & LATCH PLATE CHAFED. R & R LATCH PLATE IAW SRM 51-42-06 & SRM 51-42-13. BLENDED HINGE BODY IAW EA 954-03625. R & R HINGE LEVER IAW SRM 51-42-02 0.003 MATERIAL REMOVED.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 18,699 hrs · 11,979 cycles
TASK CARD NR 32346, DURING OPERATIONS CHECK OF NR 32346 EMER LIGHTS, FOUND AFT OVER WING EMER LIGHTS INOPERATIVE. R & R THE BATTERY CHARGER NR 5 PS43 IAW AMM 33-51-17-000-802-A02 & 33-51-17-400-802-A02. PERFORMED OPERATIONS TEST OF EMER POWER SUPPLY UNIT PS43 IAW AMM 33-51-17-710-801-A02. OPERATIONS TESTED GOOD.
Part: HANDLE — CRACKED (E&E DOOR) · airframe 18,699 hrs · 11,979 cycles
TASK CARD 900-53-140-508, AVIONICS DOOR HANDLE POSSIBLE CRACK ON FWD LE AT TOP. R & R AVIONICS DOOR HANDLE ASSEMBLY IAW AMM 52-42-3-000-801-A01, 52-42-03-400-801-A01 & SRM 51-42-21-001-001-A01. DRILLED NEW HANDLE IAW SRM 51-40-11-001-001-A01. INSTALLED HANDLE ASSEMBLY INTO DOOR IAW SRM 51-42-21-001-001-A01.
Part: STRIKER — CORRODED (FUSELAGE) · airframe 18,699 hrs · 11,979 cycles
TASK CARD 900-53-230-500, SERVICE DOOR LOWER SEAL STRIKER CORRODED AROUND FWD SCREW HOLES. R & R SERVICE DOOR LOWER STRIKER PLATE IAW AMM 53-21-23-00-801-A01 & 583-21-23-400-801-A01. REMOVED BRACKETS ANGLES & SEAL STRIKERS IAW SRM 51-42-06-001-001-A01. INSTALLED SERVICE DOOR STRIKER PLATE IAW SRM 51-42-06. INSTALLED PROTECTOR PLATE IAW AMM 53-21-23. INSTALLED SERVICE DOOR FITTINGS IAW AMM 53-21-27. LEAK CHECK OF SERVICE DOOR GOOD IAW AMM 52-00-00-790-801-A01.
Part: PLATE — CHAFED (LT COWLING) · airframe 18,699 hrs · 11,979 cycles
TASK CARD 900-71-430-100, LEFT ENG LOWER CORE COWL BLOW OUT DOOR HINGE & LATCH PLATE CHAFED. R & R LATCH PLATE IAW SRM 51-42-06 & SRM 51-42-13. BLENDED HINGE BODY IAW EA 954-03625. R & R HINGE LEVER IAW SRM 51-42-02 0.003 MATERIAL REMOVED.
Part: HANDLE — CRACKED (PAX DOOR) · airframe 18,699 hrs · 11,979 cycles
TASK CARD 900-52-810-104, POSSIBLE CRACK ON PAX DOOR, INNER HANDLE BY TAPER PIN. R & R INNER HANDLE ON PAX DOOR IAW AMM 52-11-02. PERFORMED OPERATION CHECK OF PAX DOOR IAW AMM 52-11-00. OPERATIONS CHECKED GOOD.
Part: FAIRING — GOUGED (RT ENGINE) · airframe 18,699 hrs · 11,979 cycles
TSK CARD, RIGHT ENG HINGE LINE FAIRING 443BB GOUGED. REPLACE RT ENG HINGE LINE FAIRING 443BB IAW SRM 54-12-01, 51-42-13, 51-40-11 & 51-42-06.
Part: CHANNEL — DAMAGED (LT MLG WW) · airframe 18,699 hrs · 11,979 cycles
TASK CARD 900-53-900-106, LEFT WHEEL BIN SECURE BRACKET HOLE ELONGATED. R & R LT WW CHANNEL ASSEMBLY IAW SRM 51-42-21.
Part: FAIRING — CHAFED (LT ENGINE) · airframe 18,699 hrs · 11,979 cycles
TASK CARD 900-54-430-300, LEFT ENG AFT LOWER HINGE LINE FAIRING CHAFED. REMOVED STIFFENERS FROM LT ENG AFT LOWER HINGE LINE FAIRING. LOCATED & DRILLED FASTENER HOLES IN NEW FARING SKIN & INSTALLED STIFFENERS ON NEW SKIN IAW SRM 51-42-06, SRM 51-40-11 & SRM 51-42-13.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 18,699 hrs · 11,979 cycles
TASK CARD 900-53-900-514, MAIN CABIN RT SIDE SEAT RAILS FROM FS 669.40 TO 977.00 HAVE EIGHT CORRODED & NICKED PLACES. ALL EIGHT PLACES ARE MARKED WITH YELLOW DOTS NUMBERED 24 - 65. R & R THE RT SIDE SEAT RAIL BETWEEN FS 785.15 & 84700-116.0 IAW AMM 53-00-49-000-801-A01-A07 & 53-00-49-400-801-A07.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 18,699 hrs · 11,979 cycles
TASK CARD 900-53-230-500, UPON REMOVAL OF GALLEY SERVICE DOOR LOWER SEAL STRIKER ON OPS 32315, DISCOVERED CORROSION ON SILL MOUNTING ANGLE. R & R GALLEY SERVICE DOOR SILL MOUNTING ANGLE IAW SRM 51-42-06 & SRM 51-40-11.
Part: PANEL — CRACKED · airframe 18,699 hrs · 11,979 cycles
TASK CARD 900-54-420-300, RIGHT HINGE LINE PANEL 443BT CRACKED. RE-SKINNED PANEL 443BT IAW SRM 51-42-06, 54-21-01 & 51-40-11.
Part: PLATE — CORRODED (FUSELAGE) · airframe 18,699 hrs · 11,979 cycles
TASK CARD 900-53-140-509, SILL PLATE AT FS 280.00, RBL 36.00 CORRODED. REPAIRED FLOOR SILL AT FS 280, RBL 36 IAW SRM 53-21-43.
Part: LIGHT — DETACHED (CABIN) · airframe 18,684 hrs · 11,965 cycles
FLOOR EXIT LIGHT STRIP AT 12C IS LOOSE & DETACHED. REATTACHED EMER LIGHT STRIP AT 12C IAW AMM 33-51-01. ACFT OK FOR SERVICE.
Part: LIGHT — MISSING (CABIN) · airframe 17,482 hrs · 11,139 cycles
TWO SECTIONS OF EMERGENCY LIGHTS MISSING IN CABIN. REPLACED SECTIONS IAW 33-51-01. OPS CHECKS GOOD.
Part: LIGHT — MISSING (CABIN) · airframe 17,482 hrs · 11,139 cycles
EMERGENCY LIGHT STRIP MISSING NEAR SEAT 12B. INSTALLED NEW LIGHT STRIP. OK FOR SERVICE.
2014
Part: LIGHT — MISSING (CABIN) · airframe 17,117 hrs · 10,889 cycles
EMERGENCY FLOOR TRACK LIGHTING STRIP IS MISSING NEAR SEAT 12B. REPLACED EMER STRIP AT 12B IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 16,175 hrs · 10,265 cycles
FLASHLIGHT INOPERATIVE. BEHIND AFT CABIN JUMP SEAT. R & R BATTERY OF EMER FLASHLIGHT IAW AMM 25-60-11. LIGHT WORKS, RED LIGHT FLASHES OPERATIONS CHECKED GOOD.
Part: SLEEVE — OUT OF ALIGNMENT (LT MLG) · airframe 16,112 hrs · 10,217 cycles
ON DEPART AT APPROX 160 KTS THE LG LEVER WAS PLACED IN POS, THE LT MAIN GEAR IND TURNED YELLOW DURING TRANSIT, BUT TURNED RED AFTER THE NOSE & RT MAIN IND SHOWED UP. MASTER WARNING. NON NORMAL CHECKLIST FOR GEAR DISAGREE UP WAS PERFORMED & COMPLETED. LANDED AT APPROX 70,000 LBS TOUCHING DOWN AT APPROX 300 FT DOWN ON VSI. 4 GEAR PINS ARE ON BOARD. NO PIN IN WELL WHICH WAS CHECKED BY FIRST OFFICER DURING PREFLIGHT INSPECTION. FOUND UP LOCK TRAVEL LIMITED BY MISALIGNED BOLT SLEEVE. REALIGNED BOLT SLEEVE IAW AMM 32-32-01 PG 414 GAP CHECKED GOOD IAW AMM 32-32-01 FIG 402. PERFORMED EXTENSION & RETRACTION OPERATIONS CHECKED IAW AMM TASK 32-30-00-710-801, CHECKED GOOD NO OTHER DEFECT NOTED AT THIS TIME.
2013
Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 15,012 hrs · 9,517 cycles
FLASHLIGHT AT EXTRA JUMPSEAT NOT FLASHING. R & R NR 3 FLASHLIGHT AND HOLDER, IAW AMM 25-61-02. OPS CHECKED GOOD.
Part: CONNECTOR — LOOSE (CABIN) · airframe 14,957 hrs · 9,486 cycles
MID CABIN CEILING FWD FACING EMERGENCY EXIT SIGN INOPERATIVE. TROUBLE SHOT & FOUND CONNECTOR J5452 WITH LOOSE CONNECTOR. SECURED & REPINED CONNECTOR J5452 IAW CRJ 900 ESPM 20-26-38. OPERATIONS CHECKED GOOD, OKAYED FOR SERVICE.
Part: LIFE VEST — MISSING (CABIN) · airframe 14,911 hrs · 9,453 cycles
WHILE PERFORMING CRJ 900 EMERGENCY EQUIPMENT INSPECTION STICKER CHECK FOUND THREE INFANT LIFE VEST MISSING. DEFERRED THREE INFANT LIFE VEST IAW NEF N25-21-9A, ENTERED INTO MM02. PLACARD INSTALLED CONTROL 2348585-2, MOC NOTIFIED 53212 JMK 12540. INSTALLED THREE INFANT LIFE VEST PN P0640-101. REMOVED FROM MM02 & MXC NOTIFIED 96096.
Part: SEAL — MISSING (PBE) · airframe 14,717 hrs · 9,326 cycles
AFT PBE MISSING SEALS, INSPECTED AFT PBE AND INSTALLED NEW SEALS, IAW AMM 35-31-06.
Part: STRUCTURE — GOUGED (BS 913-927) · airframe 14,625 hrs · 9,272 cycles
GOUGE AT BS 913-927, STR 27. REPAIRED GOUGE DAMAGE IAW EO R53508.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 14,625 hrs · 9,272 cycles
RT SEAT TRACK UNDER INBD SIDE OF LAVATORY CORRODED. R & R RT SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
Part: GUIDE — CHAFED (PAX DOOR) · airframe 14,625 hrs · 9,272 cycles
MAIN ENTRY DOOR UPPER FWD GUIDE PLATE IS CHAFED. REPAIRED MAIN ENTRY DOOR UPPER FWD GUIDE PLATE IAW EOR 5098.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 14,625 hrs · 9,272 cycles
MAIN ENTRY DOOR AFT DRAG ANGLE IS CRACKED. REPAIRED MAIN ENTRY DOOR AFT DRAG ANGLE IAW SRM 52-11-04-002-A01.
Part: RETAINER — BENT (CARGO DOOR) · airframe 14,625 hrs · 9,272 cycles
FWD CARGO DOOR, LOWER INNER SEAL RETAINER IS BENT. R & R SEAL RETAINER IAW AMM 52-35-07. LEAK CHECKED GOOD IAW AMM 52-00-00.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 14,625 hrs · 9,272 cycles
INTERCOSTAL AT RBL 2, BETWEEN FS 349 AND 364, CORRODED. R & R INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.
Part: ARM — CHAFED (PAX DOOR) · airframe 14,625 hrs · 9,272 cycles
MAIN ENTRY DOOR, UPPER FWD PULL IN ARM IS CHAFED. R & R PULL IN ARM IAW AMM 52-11-00. OPS CHECKED GOOD IAW AMM 52-11-00-710-801.
Part: GUIDE — CHAFED (PAX DOOR) · airframe 14,625 hrs · 9,272 cycles
MAIN ENTRY DOOR UPPER AFT GUIDE PLATE IS CHAFED. REPAIRED MAIN ENTRY DOOR UPPER AFT GUIDE PLATE IAW EO R52098, MM 409 410871.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 14,625 hrs · 9,272 cycles
FLOOR SUPPORT CORRODED. REMOVED CORRODED FLOOR SUPPORT AND REPLACED WITH SERVICEABLE PART IAW SRM 51-41-02.
Part: RETAINER — BENT (CARGO DOOR) · airframe 14,625 hrs · 9,272 cycles
MID CARGO DOOR, LOWER INNER SEAL RETAINER IS BENT. R & R SEAL RETAINER IAW SRM 51-42-06. LEAK CHECKED GOOD IAW AM 52-00-00.
Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 14,625 hrs · 9,272 cycles
FWD CARGO DOOR, OUTER LOWER SEAL RETAINER IS GOUGED AND DENTED. REPLACED FWD CARGO DOOR OUTER LOWER SEAL RETAINER IAW SRM 51-42-06. LEAK CHECKED GOOD IAW AMM 52-00-00.
Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 14,625 hrs · 9,272 cycles
MID CARGO DOOR, LOWER OUTER SEAL RETAINER IS GOUGED AND DENTED. R & R MID CARGO DOOR LOWER OUTER SEAL RETAINER IAW SRM 51-42-06. LEAK CHECKED GOOD IAW AMM 52-00-00.
Part: HANDLE — CRACKED (PAX DOOR) · airframe 14,625 hrs · 9,272 cycles
MAIN ENTRY DOOR INNER HANDLE IS CRACKED. R & R PAX DOOR INNER HANDLE IAW AMM 52-11-02. OPS CHECKED GOOD IAW AMM 52-11-00-710-801.
Part: FLOORBEAM — CRACKED (BS 274) · airframe 14,625 hrs · 9,272 cycles
FLOORBEAM IS CRACKED AT FS 274 LBL 12. REPAIRED FLOORBEAM IAW EO REF MM 409 41137.
Part: STRINGER — CORRODED (BS 310) · airframe 14,625 hrs · 9,272 cycles
STRINGER 25L IS CORRODED AT FS 310. REPLACED STRINGER FS 280-333 IAW SRM 51-21-11, 51-42-21.
Part: FRAME — CORRODED (BS 319.7) · airframe 14,625 hrs · 9,272 cycles
FRAME AT FS 319.70 CORRODED BETWEEN S26-27R. REMOVED CORROSION AND RESTORED FINISH IAW EO R53277. ,
Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 14,625 hrs · 9,272 cycles
STRINGER SPLICE 26R IS CORRODED FS 333. REPLACED STRINGER SPLICE IAW SRM 51-42-06, 51-42-21.
Part: STRINGER — CORRODED (BS 280-295) · airframe 14,625 hrs · 9,272 cycles
STRINGER 26L IS CORRODED BETWEEN FS 280 AND 295. REPLACED STRINGER BS 280-333 IAW SRM 51-42-06, 51-42-21.
Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 14,625 hrs · 9,272 cycles
STRINGER SPLICE 25L, FS 333 CORRODED. REPLACED STRINGER SPLICE IAW SRM 51-42-06, 51-42-21.
Part: DOUBLER — CORRODED (BS 295-310) · airframe 14,625 hrs · 9,272 cycles
TCAS ANTENNA DOUBLER, BETWEEN FS 295 AND 310, CORRODED. REPLACED ANTENNA DOUBLER IAW SRM 51-42-06, 51-42-21.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 14,625 hrs · 9,272 cycles
INTERCOSTAL AT STRINGER 26L, BETWEEN FS 349 AND 364, CORRODED. REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21.
Part: STRINGER — CORRODED (BS 333-364) · airframe 14,625 hrs · 9,272 cycles
LONGERON 25R CORRODED FROM FS 333 TO 364. REPLACED STRINGER IAW SRM 51-42-06, 51-42-21.
Part: STRINGER — CORRODED (BS 333-364) · airframe 14,625 hrs · 9,272 cycles
STRINGER 26R CORRODED FROM FS 333 TO 364. REPLACED STRINGER IAW SRM 51-42-06, 51-42-21.
Part: STRINGER — CORRODED (BS 295-310) · airframe 14,625 hrs · 9,272 cycles
STRINGER 25R IS CORRODED BETWEEN FS 295 AND 310. REPLACED STRINGER FS 280-333 IAW SRM 51-42-06, 51-42-21.
Part: FRAME — CORRODED (BS 295) · airframe 14,625 hrs · 9,272 cycles
FS 295 FRAME CORRODED BETWEEN S26-27R. REMOVED CORROSION AND RESTORED FINISH IAW EO R53277.
Part: ACCESS PANEL — CRACKED (NR 1 NACELLE) · airframe 14,625 hrs · 9,272 cycles
NR 1 ENGINE ACCESS PANEL 433BT IS CRACKED. FABRICATED NEW ACCESS PANEL IAW SRM 51-24-21 AND SRM 51-40-11.
Part: FRAME — CORRODED (BS 310) · airframe 14,625 hrs · 9,272 cycles
FRAME FLANGE CORRODED FS 310 BETWEEN STRINGERS 25 & 26R. R & R IAW SRM 51-52-16 AND EO R53277.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 14,625 hrs · 9,272 cycles
INTERCOSTAL AT LBL 2, BETWEEN FS 349 AND 364 CORRODED. REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21.
Part: FAIRING — GOUGED (RT NACELLE) · airframe 14,625 hrs · 9,272 cycles
RT ENGINE LOWER AFT HINGE LINE FAIRING 443BB GOUGED. FABRICATED NEW HINGE LINE FAIRING IAW SRM 51-24-21 AND SRM 51-40-11.
Part: FRAME — CORRODED (BS 310) · airframe 14,625 hrs · 9,272 cycles
FS 310, FRAME CORRODED BETWEEN S25-26L. REMOVED CORROSION AND RESTORED FINISH IAW SRM 51-21-11, 51-25-16 AND IAW EO R53277.
Part: ACCESS PANEL — DAMAGED (NR 2 NACELLE) · airframe 14,625 hrs · 9,272 cycles
NR 2 ENGINE ACCESS PANEL 443BT CRACKED AND GOUGED. FABRICATED NEW ACCESS PANEL IAW SRM 51-24-21 AND SRM 51-40-11.
Part: FLOORBEAM — CRACKED (BS 274) · airframe 14,625 hrs · 9,272 cycles
FLOORBEAM CRACKED FS 274 RBL 12. REPAIRED FLOORBEAM IAW MM 409 41138.
Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 14,625 hrs · 9,272 cycles
STRINGER SPLICE 25R CORRODED AT FS 333. REPLACED STRINGER SPLICE IAW SRM 51-42-06, 51-42-21.
Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 14,625 hrs · 9,272 cycles
STRINGER SPLICE 26L AT FS 333 CORRODED. REPLACED STRINGER SPLICE IAW SRM 51-42-06, 51-42-21.
Part: STRINGER — CORRODED (BS 295-333) · airframe 14,625 hrs · 9,272 cycles
STRINGER 26R IS CORRODED BETWEEN FS 295 AND 333. REPLACED STRINGER FS 280-333 IAW SRM 51-42-06, 51-42-21.
Part: STRINGER — CORRODED (BS 333-364) · airframe 14,625 hrs · 9,272 cycles
STRINGER 26L CORRODED FROM FS 333 TO 364. REPLACED STRINGER IAW SRM 51-42-06, 51-42-21.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 14,625 hrs · 9,272 cycles
INTERCOSTAL AT STRINGER 26R, BETWEEN FS 349 AND 364 IS CORRODED. REPLACED INTERCOSTAL IAW SRM 51-42-06, 51-42-21.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,625 hrs · 9,272 cycles
LEFT BS 280 FLOORBEAM CORRODED. R & R FLOORBEAM IAW EO R53505, R53117, & R53127.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,625 hrs · 9,272 cycles
LT BS 280 FLOORBEAM CAP DAMAGED. R & R FLOORBEAM ANGLE IAW SRM 57-42-06.
Part: SKIN — CORRODED (FUSELAGE) · airframe 14,625 hrs · 9,272 cycles
FUSELAGE SPACER CORRODED BENEATH NR 2 RADIO ALTIMETER TRANSMIT ANTENNA. R & R WITH NEW ANTENNA BASE FOR NR 2 RADIO ALT TRANSMIT ANTENNA IAW SRM 51-42-06 AND 51-40-11.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,625 hrs · 9,272 cycles
RT 280 FLOORBEAM CAP DAMAGED. R & R FLOORBEAM ANGLE IAW SRM 57-42-06.
Part: STRAP — CRACKED (FAIRING PANEL) · airframe 14,625 hrs · 9,272 cycles
FAIRING PANEL 196DR STRAP CRACKED. R & R STRAP IAW SRM 51-42-13.
Part: SKIN — CORRODED (FSUELAGE) · airframe 14,625 hrs · 9,272 cycles
FUSELAGE SPACER CORRODED BENEATH NR 1 RADIO ALTIMETER TRANSMIT ANTENNA. R & R WITH NEW NR 1 RADIO ALT TRANSMIT ANTENNA BASE IAW SRM 51-42-06 AND 51-40-11.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,625 hrs · 9,272 cycles
RT BS 280 FLOORBEAM CORRODED. R & R FLOORBEAM IAW EO R53505, R53117 AND R53127.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,625 hrs · 9,272 cycles
FLOORBEAM ANGLE FS 280 CORRODED. R & R FLOORBEAM ANGLE IAW SRM 57-42-06.
Part: SKIN — CORRODED (FUSELAGE) · airframe 14,625 hrs · 9,272 cycles
FUSELAGE SPACER CORRODED BENEATH NR 2 RADIO ALTIMETER RECEIVE ANTENNA. R & R WITH NEW ANTENNA BASE FOR NR 2 RADIO ALT RECEIVE IAW SRM 51-40-11.
Part: VANE — CHAFED (LT WING TE FLAP) · airframe 14,625 hrs · 9,272 cycles
LEFT WING INBD FLAP VANE IB L/E PANEL IS CHAFED. REPAIRED LT WING INBD FLAP VANE INBD L/E PANEL IAW EA CRJ 957-01976, REF MM409 411313.
Part: VANE — CHAFED (RT WING TE FLAP) · airframe 14,625 hrs · 9,272 cycles
RIGHT WING INBD FLAP VANE INBD L/E PANEL IS CHAFED. REPAIRED RT WING INBD FLAP VANE INBD L/E PANEL IAW EA CRJ2 57-01983, REF MM409 411312.
Part: MOUNT — WORN (RUB PAD) · airframe 14,625 hrs · 9,272 cycles
LT AFT CORE COWL RUB PAD MOUNT BLOCK WORN. R & R LT AFT CORE COWL RUB PAD MOUNT BLOCK IAW SRM 54-13-00.
Part: SKIN — CORRODED (FUSELAGE) · airframe 14,625 hrs · 9,272 cycles
ON REMOVAL OF NR 2 RADIO ALT TRANSMIT ANTENNA SPACER, CORROSION FOUND ON FUSELAGE SKIN. REMOVED CORROSION ON SKIN AND IS IN LIMITS IAW SRM 53-61-01.
Part: SKIN — CORRODED (FUSELAGE) · airframe 14,625 hrs · 9,272 cycles
ON REMOVAL OF NR 1 RADIO ALT TRANSMIT ANTENNA SPACER, CORROSON FOUND ON FUSELAGE SKIN. REMOVED CORROSION ON SKIN AND IS IN LIMITS IAW SRM 53-61-01.
Part: SKIN — CORRODED (FUSELAGE) · airframe 14,625 hrs · 9,272 cycles
ON REMOVAL OF NR 2 RADIO ALT RECEIVE ANTENNA SPACER, CORROSION FOUND ON FUSELAGE SKIN. REMOVED CORROSION ON SKIN AND IS IN LIMITS IAW SRM 53-61-01.
Part: MOUNT — WORN (RUB PAD) · airframe 14,625 hrs · 9,272 cycles
RT AFT CORE COWL RUB PAD MOUNT BLOCK WORN. REMOVED AND INSTALLED STANDOFF RUB PAD MOUNT ON RT AFT CORE COWL IAW SRM 51-42-06.
Part: ARM — GOUGED (CARGO DOOR) · airframe 14,625 hrs · 9,272 cycles
FWD CARGO DOOR, AFT LOWER HINGE ARM IS GOUGED. REMOVED GOUGE ON FWD CARGO AFT LOWER HINGE ARM AND IS IN LIMITS IAW EA CRJ 952-01974.
Part: WEB — CRACKED (PAX DOOR STEP) · airframe 14,625 hrs · 9,272 cycles
MAIN ENTRY DOOR AFT AIRSTAIR WEB IS CRACKED AT TOP STEP RISER. REPAIRED MAIN ENTRY DOOR AFT AIRSTAIR WEB IAW REO 670-52-1-104. REM MM 409 410868.
Part: ACCESS PANEL — CORRODED (PAX DOOR) · airframe 14,625 hrs · 9,272 cycles
MAIN ENTRY DOOR ACCESS PANEL 832CL IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06 PANEL FOUND TO BE IN LIMITS IAW EA CRJ952-01982.
Part: WEB — CHAFED (CARGO DOOR) · airframe 14,625 hrs · 9,272 cycles
MID CARGO DOOR INNER WEB IS CHAFED ON FWD & AFT LOWER CORNERS. BLENDED CHAFE ON MID CARGO INNER WEB ON FWD AND AFT CORNERS AND IS IN LIMITS IAW EA, MM 409 410858. CR3213-5-3, B51107.
Part: SKIN — CORRODED (FUSELAGE) · airframe 14,625 hrs · 9,272 cycles
UPON REMOVAL OF TCAS ANTENNA CORROSION FOUND ON FUSELAGE SKIN. REMOVED CORROSION IAW SRM 51-21-06 SKIN FOUND TO BE IN LIMITS IAW EA CRJ953-01981.
Part: TAB — CHAFED (RT PANEL) · airframe 14,625 hrs · 9,272 cycles
RIGHT PANEL 622CB TABS ARE CHAFED. REMOVED CHAFE IAW SRM 51-12-00 TABS FOUND TO BE IN LIMITS IAW EA CRJ957-01977.
Part: WEB — CHAFED (CARGO DOOR) · airframe 14,625 hrs · 9,272 cycles
FWD CARGO DOOR INNER WEB IS CHAFED ON FWD & AFT LOWER CORNERS. BLENDED CHAFE ON FWD CARGO INNER WEB ON FWD AND AFT CORNERS AND IS IN LIMITS IAW EA CRJ952-01978.
Part: SKIN — CHAFED (LT NACELLE) · airframe 14,625 hrs · 9,272 cycles
LEFT AFT CORE COWL L/E CHAFED. REPAIRED LT AFT CORE COWL L/E IAW SRM 54-13-00.
Part: SKIN — CHAFED (RT NACELLE) · airframe 14,625 hrs · 9,272 cycles
RT AFT CORE COWL L/E CHAFED. REPAIRED RT AFT CORE COWL L/E IAW SRM 54-13-00.
Part: ARM — GOUGED (CARGO DOOR) · airframe 14,625 hrs · 9,272 cycles
FWD CARGO DOOR, FWD LOWER HINGE ARM IS GOUGED. REMOVED GOUGE ON FWD CARGO DOOR FWD LOWER HINGE ARM AND IS IN LIMITS IAW EA CRJ 952-01974.
Part: PANEL — CHAFED (WING) · airframe 14,625 hrs · 9,272 cycles
PANEL 684GB IS CHAFED. REPAIRED PANEL 684GB IAW SRM 57-52-01.
Part: PANEL — CHAFED (WING) · airframe 14,625 hrs · 9,272 cycles
PANEL 684LB IS CHAFED. REPAIRED PANEL 684LB IAW SRM 57-52-01.
Part: HINGE — GOUGED (PAX DOOR) · airframe 14,625 hrs · 9,272 cycles
MAIN ENTRY DOOR HINGE (ACFT SIDE) IS GOUGED, MIGRATED ROLL PIN, ON AFT SIDE. REPAIRED MAIN ENTRY DOOR HINGE (ACFT SIDE) ON AFT END IAW SRM 53-21-23.
Part: PANEL — CHAFED (WING) · airframe 14,625 hrs · 9,272 cycles
PANEL 684DB IS CHAFED. REPAIRED PANEL 684DB IAW SRM 57-52-01.
Part: PANEL — CHAFED (WING) · airframe 14,625 hrs · 9,272 cycles
PANEL 684JB IS CHAFED. REPAIRED PANEL 684KB IAW SRM 57-52-01.
Part: SKIN — DENTED (PAX DOOR) · airframe 14,625 hrs · 9,272 cycles
MAIN ENTRY DOOR UPPER FWD AND AFT CORNER PANELS ARE DENTED AND HAVE DAMAGED FASTENERS. R & R WITH NEW FASTENERS ON FWD AND AFT CORNERS IAW SRM 51-42-13 AND MEASURED DENTS IN LIMITS IAW SRM 52-11-01.
Part: PANEL — CHAFED (WING) · airframe 14,625 hrs · 9,272 cycles
PANEL 684EB IS CHAFED. LOCATED AND DRILLED NEW REPLACEMENT PANEL IAW SRM 51-40-11.
Part: PANEL — CHAFED (WING) · airframe 14,625 hrs · 9,272 cycles
PANEL 684AB IS CHAFED. REPAIRED PANEL 684AB IAW SRM 57-52-01.
Part: SKIN — CHAFED (RT WING SLAT) · airframe 14,625 hrs · 9,272 cycles
RT WING SLAT 1 OTBD END UNDERSIDE IS CHAFED. REPAIRED RT WING NR 1 SLAT OTBD END T/E IAW SRM 57-42-01, MM 409 410857.
Part: HINGE — CORRODED (DOOR STEP) · airframe 14,625 hrs · 9,272 cycles
PAX DOOR TOP FOLDING STEP, FUSELAGE SIDE HINGE CORRODED. REPLACED PAX DOOR TOP FOLDING STEP HINGE IAW SRM 51-40-11.
Part: WIRE — PULLED (EMERGENCY LIGHT) · airframe 14,625 hrs · 9,272 cycles
RIGHT AFT OVER WING EMERGENCY EXIT LIGHT WIRE PULLED OUT OF LIGHT. INSTALLED NEW CONTACT TO DS56 IAW ESPM 20-16-00. OP TEST OF EXTERNAL EMERGENCY, GOOD IAW AMM 33-51-00.
Part: LIGHT — MISSING (GALLEY) · airframe 14,582 hrs · 9,246 cycles
FWD LEFT GALLEY EMERGENCY LIGHT IS MISSING. REPLACED MISSING EMERGENCY LIGHT IAW AMM 33-51-01.
Part: LIGHT — MISSING (CABIN) · airframe 14,439 hrs · 9,164 cycles
EMERGENCY LIGHT MISSING AT ROW 13 A & B. REPLACED LIGHT IAW AMM 33-51-01. OK FOR SERVICE.
2011
Part: UNKNOWN — DAMAGED · airframe 9,228 hrs · 5,959 cycles
DURING INCORPORATION OF GREO 670-53-11-509 HOLE AT FS 193, RT SIDE WAS DOUBLE DRILLED. REO 690-53-11-306. INCORPORATED AND COMPLIED WITH EO R53134 WHICH ADDRESSES ABOVE GREO AND DEVIATION.
Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 8,853 hrs · 5,726 cycles
DURING LINE CHECK FOUND CRACKS ON AFT SIDE OF PAX DOOR. INSPECTED IAW REO 690-52-11-153. PAX DOOR OPERATES NORMALLY AND PRESSURIZATION CHECK IAW AMM 52-00-00. FOUND ACFT SAFE FOR 1 TIME FERRY FLIGHT FOR FURTHER INSPECTION AND REPAIR OF PAX DOOR. REPAIRED PAX DOOR IAW EO R52026, R2022. ALL CHECKS GOOD.
Part: LIGHT — MISSING (CABIN) · airframe 8,742 hrs · 5,660 cycles
GLOW STRIP ON FLOOR OF GALLEY (NEAR CURTAIN) IS MISSING. INSTALLED FLOOR TRACK LIGHTING STRIP, PN PL88-910LH00.
Part: LIGHT — MISSING (CABIN) · airframe 8,471 hrs · 5,502 cycles
EMERGENCY LIGHTING IN FRONT GALLEY MISSING. INSTALLED NEW LIGHTING STRIP PN PL88-900LH00 IAW 33-51-01.
Part: LIGHT — MISSING (CABIN) · airframe 8,214 hrs · 5,352 cycles
EMERGENCY PATH STRIP MISSING ON LT SIDE OF GALLEY. INSTALLED NEW FLOOR TRACK LIGHTING AS REQUIRED IAW MM 33-20 ALL CHECKS GOOD AT THIS TIME.
2009
Part: STRIP — MISSING (CABIN) · airframe 3,386 hrs · 2,484 cycles
MISSING EMERGENCY FLOOR PATH STRIP AT SEAT 12AB. REPLACED EMERGENCY FLOOR PATH STRIP AT SEAT 12AB.