N925XJ
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
191 reports on file, 2008-07-13 – 2026-07-28.
Part: LUG — DAMAGED (ZONE 600) · airframe 39,948 hrs · 28,550 cycles
FABRICATE OVERSIZE BUSHINGS FOR LUGS R1, R2, R5 & R6. LUG R1 WAS REWORKED AND BUSHINGS OVERSIZE FOR LUGS R2, R5 & R6 WERE FABRICATED PER REO 670-57-61-237 REV.--
Part: LUG — CORRODED (ZONE 500) · airframe 39,948 hrs · 28,550 cycles
CORROSION AND WEAR WAS FOUND ON LUG BORE ON AIL STA 336.4015 (LUG L1), 337.657 (LUG L2), 342.911 (LUG L5), 344.1665 (LUG L6) AT LH AILERON. CORROSION AND WEAR ON LUG BORE ON AIL STA 336.4015 (LUG L1), 337.657 (LUG L2), 342.911 (LUG L5), 344.1665 (LUG L6) AT LH AILERON WERE REPAIRED PER REO 670-59-61-237 REV:-- & CLEAN PER SRM 51-26-00-001-001-A01 CLEANING
Part: PROTECTOR — CORRODED (ZONE 200) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-A01, THEREFORE NEW FLOOR PROTECTOR (4EAS) WERE DRILLED, TREATED, PAINTED AND NUTS INSTALLED PER CRJ-900 SRM 51-40-11-001-001-A01, CRJ-900 SRM 51-21-11-001-001-A01, SRM 51-25-06-001-001-A01, SRM 51-25-16-001-001-A01, CRJ-900 SRM 51-42-10-001-001-A01 AND INSTALLED UNDER NRC 00255
Part: BRACKET — CORRODED (ZONE 200) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-A01, THEREFORE NEW FLOOR PROTECTOR (4EAS) WERE DRILLED, TREATED, PAINTED AND NUTS INSTALLED PER CRJ-900 SRM 51-40-11-001-001-A01, CRJ-900 SRM 51-21-11-001-001-A01, SRM 51-25-06-001-001-A01, SRM 51-25-16-001-001-A01, CRJ-900 SRM 51-42-10-001-001-A01 AND INSTALLED UNDER NRC 00255
Part: BRACKET — CORRODED (ZONE 200) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-A01, THEREFORE NEW FLOOR PROTECTOR (4EAS) WERE DRILLED, TREATED, PAINTED AND NUTS INSTALLED PER CRJ-900 SRM 51-40-11-001-001-A01, CRJ-900 SRM 51-21-11-001-001-A01, SRM 51-25-06-001-001-A01, SRM 51-25-16-001-001-A01, CRJ-900 SRM 51-42-10-001-001-A01 AND INSTALLED UNDER NRC 00255
Part: WEB — CORRODED (ZONE 200) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE CORROSION ON WEB FLOOR PROTECTOR (4EAS) AT SERVICE DOOR SURROUND STRUCTURE WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND CRJ-900 SRM 53-00-00-101-001-A01, THEREFORE NEW FLOOR PROTECTOR (4EAS) WERE DRILLED, TREATED, PAINTED AND NUTS INSTALLED PER CRJ-900 SRM 51-40-11-001-001-A01, CRJ-900 SRM 51-21-11-001-001-A01, SRM 51-25-06-001-001-A01, SRM 51-25-16-001-001-A01, CRJ-900 SRM 51-42-10-001-001-A01 AND INSTALLED UNDER NRC 00255
Part: SEAL — WORN (ZONE 500) · airframe 39,948 hrs · 28,550 cycles
LT WING TRAILING EDGE P-SEAL WORN BELOW MFS LOWER TRAILIND EDGE. LT WING TRAILING EDGE P-SEAL ON MFS LOWER TRAILIND EDGE WAS REPLACED PER CRJ-900 AMM 57-50-07 (CONFIG A01)
Part: FITTING — CORRODED (ZONE 200) · airframe 39,948 hrs · 28,550 cycles
CORROSION FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1. SUMMARY OF NRC 00306: NEW FLOOR FITTING P/N: CDSP2019-7C-760 IN AFT ACCESS 108 (1EA) ON GALLEY 1. WAS REPLACED PER SAFRAN CMM 25-33-67 REV. NO 10 DATED JUN 20/22
Part: FITTING — CORRODED (ZONE 200) · airframe 39,948 hrs · 28,550 cycles
CORROSION FLOOR FITTING IN FWD ACCESS 306 (1EA) ON GALLEY 3. SUMMARY OF NRC 00304: NEW FLOOR FITTING P/N: CDSP2019-7C-650 IN FWD ACCESS 306 (1EA) ON GALLEY 3. WAS REPLACED PER ZODIAC AEROSPACE CMM 25-33-18 REV NO 5 DATED MAY 15/15
Part: FITTING — CORRODED (ZONE 200) · airframe 39,948 hrs · 28,550 cycles
CORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. SUMMARY OF NRC 00303: NEW FLOOR FITTING P/N: CDSP2019-7C-620 IN FWD ACCESS 107 (1EA) ON GALLEY 1. WAS REPLACED PER SAFRAN CMM 25-33-67 REV. NO 10 DATED JUN 20/22
Part: HINGE — CORRODED (ZONE 800) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON STEP DOOR HINGE FWD, CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA STEP DOOR HINGE CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, AND STEP DOOR HINGE FWD AT AFT BAGGAGE BAY DOOR AREA WAS FABRICATED PER EA NO. CRJ953-22465 REV. IR AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
Part: HINGE — CORRODED (ZONE 800) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON STEP DOOR HINGE FWD, CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA STEP DOOR HINGE CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, AND STEP DOOR HINGE FWD AT AFT BAGGAGE BAY DOOR AREA WAS FABRICATED PER EA NO. CRJ953-22465 REV. IR AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
Part: HINGE — CORRODED (ZONE 800) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON STEP DOOR HINGE FWD, CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA STEP DOOR HINGE CENTER, AFT AT AFT BAGGAGE BAY DOOR AREA WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, AND STEP DOOR HINGE FWD AT AFT BAGGAGE BAY DOOR AREA WAS FABRICATED PER EA NO. CRJ953-22465 REV. IR AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON FLOOR SILL AT FLOOOR STRUCTURE PASSENGER CABIN BTW FS 280.00 TO 319.70 FLOOR SILL AT FLOOOR STRUCTURE PASSENGER CABIN BTW FS 280.00 TO 319.70 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND CRJ900 SRM 51-42-13-001-001-A01
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON STGR 24R AND FS333.00/FS349.00. CORROSION ON STGR 24R AND FS333.00/FS349.00. WAS EVALUATED OUT LIMITS THEREFORE WAS REPAIRED PER CRJ-900 SRM 53-21-03-101-002-A04 AND SRM 53-00-03-201-001-A0
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 39,948 hrs · 28,550 cycles
CRACK ON FLOOR BEAM ANGLE RBL 12 AT FS 280.00 WAS FOUND. NEW FLOOR BEAM ANGLE RBL 12 AT FS 280.00 WAS VERIFIED PER CRJ900 SRM 53-11-43-001-001-A01 ///REPLACE WAS PERFORMED UNDER NRC 0057
Part: STUB FRAME — CORRODED (ZONE 100) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR WERE EVALUATED OUT LIMITS PER CRJ 900 SRM 51-10-06-001-001-A01 THEREFORE WERE REPLACED PER CRJ 900 SRM 51-42-20-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01
Part: FITTING — CORRODED (ZONE 200) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON FITTING APROX ON RBL12 FITTING ON RBL12 FS:290 APROX WAS REMPLACED PER. CRJ900 SRM 51-42-21-001-001-A01 6. C.
Part: STUB FRAME — CORRODED (ZONE 100) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR STUB FRAME AT FS 533.00 AND FS 549.00 APROX STGR 18 LH AT SURROUND STRUCTURE OF FWD BAGGAGE BAY DOOR WERE EVALUATED OUT LIMITS PER CRJ 900 SRM 51-10-06-001-001-A01 THEREFORE WERE REPLACED PER CRJ 900 SRM 51-42-20-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01
Part: SKIN SPLICE — CORRODED (ZONE 100) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON INTERNAL SKIN SPLICE AT FS 280.00 TO FS 282.00 FROM STGR 24RH TO 26LH CORROSION ON INTERNAL SKIN SPLICE AT FS 280.00 TO FS 282.00 FROM STGR 24RH TO 26LH WAS REMOVED PER CRJ-900 SRM SRM 51-21-06-001-001-A01 EVALUATED BTW FS 280.00 TO FS 282.00 FROM STGR 24RH TO 26RH WITHIN LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 BTW FS 280.00 TO FS 282.00 FROM STGR 26LH TO 26 RH OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 THEREFORE WAS REAPAIRED PER EA NO: CRJ953-22629 REV. IR
Part: COLLECTOR — CORRODED (ZONE 100) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON COLLECTOR TRAY CORROSION OF THE COLLECTOR TRAY WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS EVALUATED PER CRJ-900 SRM 53 -00-00-101-001-A01 AND WAS DETERMINING WITH EXCESSIVE DAMAGE. NEW COLLECTOR TRAY WAS VERIFIED PER CRJ900 AIPC 24-23-19-01 AND WILL BE INSTALLED UNDER NRC 00006.
Part: STRAP — CORRODED (ZONE 100) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON STRAP AT FAIRING 193AB. STRAP(2EAS) AT FAIRING 193AB WERE REPLACED PER SRM 51-42-10-001-001-A01 AND SRM 51-42-06-001-001-A01
Part: BRACKET — CORRODED · airframe 39,948 hrs · 28,550 cycles
CORROSION ON INTERNAL ANGLES IN REFUEL/DEFUEL PANEL AT INTERNAL AREA OF FAIRING 192AR. CORROSION ANGLE (1 EA) IN REFUEL/DEFUEL PANEL AT INTERNAL AREA OF FAIRING 192AR WERE REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 AND WAS FOUND WITHIN OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01. ANGLE (1 EA) ON REFUEL/DEFUEL PANEL AT INTERNAL AREA OF FAIRING 192AR WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON STGR 21 RH BTWN FS 364.00 TO FS 379.00 CORROSION ON STGR 21 RH BTWN FS 364.00 TO FS 379.00 WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 EVALUATED OUT LIMITS PER CRJ-900 SRM 53-21-03-101-006-A04 THEREFORES WAS REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01
Part: ANGLE — CORRODED (ZONE 800) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON MOUNITNG ANGLE OF SERVICE DOOR BTW FS 319 TO 349 AT CPAX MOUNITNG ANGLE OF SERVICE DOOR BTW FS 319 TO 349 AT CPAX WAS EVALUATED OUT OF LIMITS DUE TO EXCESIVE CORROSION PER CRJ-900 SRM 53-00-00-101-001-A01, THEREFORE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
Part: STRAP — CORRODED (ZONE 100) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON STRAP AT FAIRING 193AB. STRAP(2EAS) AT FAIRING 193AB WERE REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01 AND SRM 51-42-06-001-001-A01
Part: ACCESS PANEL — CORRODED · airframe 39,948 hrs · 28,550 cycles
CORROSION ON ACCESS PANEL 542AZ, 542BZ, 642AZ AND 642BZ. CORROSION WERE REMOVED ON ACCESS PANEL 542BZ AND 642BZ PER CRJ-900 SRM 51-21-06-001-001-A01 AND WERE FOUND WITHIN LIMITS PER CRJ-900 SRM 53-00-01-101-001-A01. ACCESS PANELS 542AZ AND 642AZ WERE REPLACED AND VERIFIED PER CRJ900 SRM 57-22-55-001-001-A01 ITEM 3A AND 4A
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON SIDE SEAT RAILS BTW STA FS379 TO FS699 STGR15LH AND STGR15RH SIDE SEAT RAILS BTW STA FS379 TO FS699 STGR15LH AND STGR15RH WERE EVALUATED OUT LIMITS PER CRJ/900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 THEREFORE WERE REPLACED PER CRJ 900 AMM 53-00-49-000-801(CONFIG A19) AND AMM 53-00-49-400-801(CONFIG A19)
Part: ROLLER — WORN (ZONE 100) · airframe 39,948 hrs · 28,550 cycles
WEAR AFT ROLLER GUIDE UPPER AT AFT BAGGAGE BAY DOOR AFT ROLLER GUIDE UPPER AT AFT BAGGAGE BAY DOOR WAS EVALUATED OUT LIMITS PER CRJ 900 SRM 53-00-00-101-001-A01 THEREFORE WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01
Part: SUPPORT ANGLE — CRACKED (ZONE 500) · airframe 39,948 hrs · 28,550 cycles
CRACK ON LH WING BRACKET SUPPORT ANGLE SS 15.50, LOWER INNER AREA. CRACK ON LH WING BRACKET SUPPORT ANGLE SS 15.50, LOWER INNER AREA WAS REPAIRED PER EA NO: CRJ957-22519 EA REV IR
Part: STRINGER — CORRODED (ZONE 100) · airframe 39,948 hrs · 28,550 cycles
CORROSION ON STGR 27 BTW FS1162.00 AND FS 1181.00 AT REAR FUSELAGE INERNAL STRUCURE. NEW STRINGER STGR 27 BTW FS1162.00 AND FS 1181.00 AT REAR FUSELAGE INERNAL STRUCURE WAS FABRICATED PER CRJ-900 DGW: MM670-38134 REV. F AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND CRJ-900 SRM 51-42-06-001-001-A01
Part: STRAP — CRACKED (SPOILER) · airframe 39,948 hrs · 28,550 cycles
CRACK ON STRAP AT GROUND SPOILERS (2EAS INB/OUT) AT LH WING AND (1EA INB) AT RH WING SPS 21.80 PROTECTOR PLATE AT SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED DUE EXCCESSIVE CORROSION AND WILL BE REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, THEREFORE NEW PROTECTOR PLATE WAS DRILLED, TREAT, PAINT AND NUTS WERE INSTALLED PER CRJ900 SRM 51-40-11-001-001-A01, CRJ-900 SRM 51-21-11-001-001-A01 AND SRM 51-25-06-001-001-A01 AND CRJ 900 SRM 51-42-06-001-001-A01
Part: STRAP — CRACKED (SPOILER) · airframe 39,948 hrs · 28,550 cycles
CRACK ON STRAP AT GROUND SPOILERS (2EAS INB/OUT) AT LH WING AND (1EA INB) AT RH WING SPS 21.80 PROTECTOR PLATE AT SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED DUE EXCCESSIVE CORROSION AND WILL BE REPLACED PER CRJ900 SRM 51-10-06-001-001-A01, THEREFORE NEW PROTECTOR PLATE WAS DRILLED, TREAT, PAINT AND NUTS WERE INSTALLED PER CRJ900 SRM 51-40-11-001-001-A01, CRJ-900 SRM 51-21-11-001-001-A01 AND SRM 51-25-06-001-001-A01 AND CRJ 900 SRM 51-42-06-001-001-A01
Part: TRACK — WORN (ZONE 800) · airframe 39,948 hrs · 28,550 cycles
WEAR LOWER AFT RAIL OF AFT BAGGAGE DOOR LOWER AFT RAIL OF AFT BAGGAGE DOOR WAS REPAIRED PER EA:CRJ953-22520 REV IR
Earlier reports · 2008–2025 · 157 reports
2025
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 36,973 hrs · 26,092 cycles
L AND R AFT EXTERIOR EMERGENCY LIGHTS INOP R/R AFT(PS38) EMERGENCY LIGHT BATTERY ASSY AND CHARGER ASSY IAW CRJ900 AMM 33-51-17 OPC GOOD
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 36,947 hrs · 26,075 cycles
FOUND EMERGENCY LIGHTING IN CABIN REAR AND EXTERNAL REAR NOT WORKING R/R EPSU BATTERY PACK PS38 IAW JOB CARD 33-900-701. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED P/N ON/OFF 2013-1ASMI S/N ON 19356 S/N OFF 19241
2024
Part: WINDSHIELD — INOPERATIVE (COCKPIT LEFT) · airframe 35,393 hrs · 24,768 cycles
DURING TAKEOFF AT ABOUT 1000 FEET, CAPTAIN'S WINDSHIELD ON LOWER LEFT SIDE STARTED SMOKING. TURNED OFF WINDSHIELD HEAT AND RETURNED TO CVG. ALSO SMELLED SMOKE FOR THE REMAINDER OF THE FLIGHT. REMOVED AND REPLACED LH CAPTAINS WINDSHIELD IAW 700/900 JC 900-56-900-901 WITH NO FURTHER DEFECTS NOTED. OPS CK GOOD
2023
Part: BEAM — CRACKED · airframe 32,884 hrs · 22,611 cycles
RBL 18 POST AT INBOARD FLANGE CRACKED. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, AND 51-42-06-001-001-A01.
Part: WEB — CRACKED · airframe 32,883 hrs · 22,610 cycles
FWD EQUIPMENT COMPARTMENT, L/H FLOOR IS CRACKED AT F.S.193. REPAIRED L/H FLOOR IN THE FWD EQUIPMENT COMPARTMENT AT F.S. 193.
2021
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,914 hrs · 20,228 cycles
RIGHT SIDE AFT MOST EMER LIGHT EXTERIOR IS INOP. REMOVED AND REPLACED RH AFT MOST OVERWING EMER. EXIT LIGHT BULB IAW AMM 33-51-15. OP/C GOOD.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,325 hrs · 19,743 cycles
EPSU BATTERY PACK DEAD (PS38). REMOVED AND REPLACED EPSU BATTERY PACK (PS38). OPERATIONAL TEST OF THE EPSU CHECK GOOD IAW AMM 33-51-17 PN OFF 2013-1A SN OFF 101377 PN ON 2013-1ASMI SN ON 12016
2020
Part: STRAP — DAMAGED (LT WING) · airframe 29,204 hrs · 19,649 cycles
LT LOWER BUTT STRAP COMMON TO LOWER WING PLANK HAS 1 EA 2ND OVERSIZE 3/8 HOLE LOCATED IN COLD WORK AREA OF TRUNNION. REPAIRED AREA, IAW REO 690-57-21-380 REV-- DATED 12/15/20.
2019
Part: STOP FITTING — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON LOWER STOP FITTING AT PASSENGER DOOR. BRACKET ASSY WAS REPLACED FOR NEW ONE (P/N: 601R38921-9) PER CRJ-900 SRM 51-42-06-001-001-A01. PAR 6C.
Part: RETAINER — DENTED (CARGO DOOR SEAL) · airframe 27,451 hrs · 18,199 cycles
SEVERAL DENTS ON LOWER RETAINER SEAL ALSO LOWER EDGE AT FWD AND MID CARGO COMPARTMENT DOOR. LOWER RETAINER SEAL FWD AND MID WERE REPLACED PER CRJ/900 AMM 52-35-07-400-802-A02, TOOL USED; TORQUEMETER P/N:QDRIVER4 S/N:0515405073 D/D:06/MAR/20.
Part: SHIELD — PERFORATED (NR 2 ENGINE) · airframe 27,451 hrs · 18,199 cycles
WEAR ON PRODUCTION DOUBLER OF PANEL BLOW OFF DOOR AT FORWARD CORE COWL ASSEMBLY UPPER RIGHT SIDE.(INNER FACE) ENGINE NR 2. A NEW BLOW OFF DOOR FIRESHIELD WAS INSTALLED PER SRM 51-22-00-001-001-A01, PAR.5, SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01, AND SRM 51-42-20-001-001-A01.
Part: INSERT — MISSING (FLOOR PANEL) · airframe 27,451 hrs · 18,199 cycles
MISSING INSERT ON FLOOR PANEL 282JRF AT AFT CARGO COMPARTMENT. THE FLOOR PANEL WAS REPLACED FOR NEW ONE IAW AMM 53-00-47.
Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON INTERCOSTAL DD6 BTW FORMER FS320.163 TO 338.963 AT PASSENGER DOOR. INTERCOSTAL DD6 BTW FORMER FS320.163 TO 338.963 AT PASSENGER DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6. C. AND SRM 51-42-21-001-001-A01 PAR. 6. C
Part: ANGLE — CORRODED (BS 319-349) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON SUPPORT MOUNTING ANGLE BTW BS 319 TO 349 AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. (W1) (CPAX). SUPPORT MOUNTING ANGLE BTW FS= 319 TO 349 AT GALLEY SERVICE DOOR LOWER WAS REPLACED PER SRM 51-42-06-001-001-A01.
Part: FLOOR SUPPORT — CORRODED (BS 1015-1047) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON FLOOR BEAM 9LBL BTW STA. FS= 1015 AND FS= 1047 AT AFT BAGGAGE BAY. FLOOR BEAM 9LBL BTW FS:1015 AND FS:1047 AT AFT BAGGAGE BAY WAS REPAIRED PER CRJ-900 SRM. 53-00-41-201-001-A03 AND CRJ-900 SRM 51-21-06-001-001-A01. CORROSION LEVEL 2.
Part: ACCESS PANEL — BROKEN (LT PYLON) · airframe 27,451 hrs · 18,199 cycles
BROKEN ACCESS PANEL 433BT AT LH PYLON. SKIN ON ACCESS PANEL 433BT AT LH PYLON WAS REPLACED FOR A NEW ONE (P/N: CN624-4230-205) PER CRJ-900 SRM 51-42-06.
Part: FRAME — CORRODED (BS 310) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON FRAME IN STA. FS= 310 BETWEEN STRG 26 LH TO 24RH AT MAIN AVIONIC COMPARTMENT. THE FRAME WAS REPAIRED PER EA NO: CRJ953-09705 REV IR,
Part: FRAME — CORRODED (BS 295) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON FRAME IN STA. FS= 295 BETWEEN STRG 25 LH TO 26RH AT MAIN AVIONIC COMPARTMENT. THE FRAME WAS REPAIRED PER EA CRJ953-09706 REV. IR.
Part: ACCESS PANEL — WORN (RT ENGINE) · airframe 27,451 hrs · 18,199 cycles
WEAR ON ACCSSES NBR 422CT AND 422DB AT RH ENGINE. THE ACCESS PANELS WERE REPLACED IAW SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED (BS 280-295) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON STRINGER 27 IN STA. FS= 280 TO FS= 295 AT MAIN AVIONICS COMPARTMENT. STRINGER WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01.
Part: INTERCOSTAL — CORRODED (BS 349-364) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R. INTERCOSTALS (4EAS) BTW FS 349-364, STGR 26L-26R WERE REPLACED PER CRJ900 SRM 51-42-06. AND SRM 51-42-20.
Part: CANISTER — LEAKING (FUEL SYSTEM) · airframe 27,451 hrs · 18,199 cycles
INITIAL INSPECTION : CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK. (AI). CANISTER WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK, WAS REPAIRED PER, REO 670-57-42-577 REV --. FUEL LEAK CHECK LH MAIN FUEL TANK WAS PERFORMED PER CRJ-900 AMM 28-11-00-790-801-A01 AND NO LEAK WAS FOUND.
Part: STRIKER — CORRODED (BS 319-349) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION AND WEAR ON LOWER STRIKER BS 319 TO 349 AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. SEAL STRIKER WAS REPLACED PER CRJ 900 SRM 51-42-06
Part: SUPPORT PLATE — CORRODED (BS 322-332) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON PROTECTION PLATE SUPPORTS IN FS= 322 AND 332 AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. PROTECTION PLATE SUPPORTS (2EA) WERE REPLACED PER CRJ-900 SRM 51-42-06 AND SRM 51-42-21
Part: CANISTER — CRACKED (RT FUEL TANK) · airframe 27,451 hrs · 18,199 cycles
CRACK IN CANISTER, WELDED NR 3 IN WS 148 AT THE RT MAIN FUEL TANK. THE CANISTER WAS REPAIRED PER, REO 670-57-42-577 REV --. FUEL LEAK CHECKED THE RH MAIN FUEL TANK WAS PERFORMED PER AMM 28-11-00-790-801-A01 AND NO LEAK WAS FOUND.
Part: SUPPORT ANGLE — CORRODED (LT MLG) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON TIRE BURST SUPPORT STRUCTURE P/N AT LH MLG AFT FACE REAR SPAR. TIRE BURST SUPPORT STRUCTURE AT LH MLG AFT FACE REAR SPAR WAS REPLACED FOR NEW ONE (P/N: CC670-10338-1) PER CRJ-900 SRM 51-42-20. FUEL LEAK CHECK LH MAIN FUEL TANK WAS PERFORMED AND NO LEAK WAS FOUND.
Part: CROSSBEAM — CRACKED (BS 280) · airframe 27,451 hrs · 18,199 cycles
AWR IN REF EO R53581 STEP 22 DURING REMOVAL OF RH DRIP TRAY, CRACK WAS FOUND ON CROSS BEAM FS 280 RBL 13. CROSS BEAM FS 280 RH SIDE WAS REPLACED PER CRJ-900 SRM 51-42-06. AND SRM 51-42-21.
Part: ANGLE — CORRODED (RT MLG) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON TIRE BURST SUPPORT STRUCTURE AT RH MLG AFT FACE REAR SPAR. TIRE BURST SUPPORT STRUCTURE AT RH MLG AFT FACE REAR SPAR WAS REPLACED FOR NEW ONE (P/N: CC670-10338-2) PER CRJ-900 SRM 51-42-20. FUEL LEAK CHECK WAS PERFORMED AND NO LEAK WAS FOUND.
Part: SUPPORT PLATE — CORRODED (BS 336-346) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON PROTECTION PLATE SUPPORTS FS= 336 AND 346 AT GALLEY SERVICE DOOR LOWER SILL, FWD WET AREA. PROTECTION PLATE SUPPORTS (2EA) WERE REPLACED PER CRJ-900 SRM 51-42-06 AND SRM 51-42-21
Part: STRINGER — CORRODED (BS 337-364) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON STRINGER 23RH IN STA. FS= 337 TO FS=364 AT MAIN AVIONICS COMPARTMENT. STRINGER 23RH IN STA. FS= 337 TO FS= 364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED (BS 280-327) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
INITIAL INSPECTION: CORROSION ON STRINGER 23RH IN STA. FS= 280 TO FS=327 AT MAIN AVIONICS COMPARTMENT. STRINGER 23RH IN STA. FS= 280 TO FS= 333 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: FRAME — CORRODED (BS 349) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON FRAME BS 349 BETWEEN STRINGERS 25L TO 24R IN THE MAIN AVIONIC COMPARTMENT. THE FRAME SECTION WAS REPLACED IAW SRM 51-42-20-001-001-A01, AND SRM 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED (BS 394-409) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON INTERCOSTALS (2EAS) BTW FS 394-409, LBL3-RBL3. INTERCOSTALS (2EAS) BTW FS 394-409, LBL3-RBL3. WERE REPLACED PER CJ900 SRM 51-42-06. AND SRM 51-42-20.
Part: STRINGER — CORRODED (BS 280-327) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
INITIAL INSPECTION: CORROSION ON STRINGER 22RH IN STA. FS= 280 TO FS=327 AT MAIN AVIONICS COMPARTMENT. STRINGER 22RH IN STA. FS= 280 TO FS= 333 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: FLOOR SUPPORT — CORRODED (BS 1015-1030) · airframe 27,451 hrs · 18,199 cycles
INITIAL INSPECTION:CORROSION ON FLOOR BEAM LBL 27 BTW STA FS:1015 AND 1030 AT AFT CARGO COMPARTMENT FLOOR BEAM LBL 27 BTW FS1015/1030 AT AFT CARGO COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-00-41-201-001-A03, SRM 51-42-20-001-001-A01 AND SRM 51-42-06-001-001-A01. (LEVEL CORROSION 2).
Part: STRUCTURE — CRACKED (GROUND POWER BOX) · airframe 27,451 hrs · 18,199 cycles
INITIAL INSPECTION: CRACK ON BOX [INTERNAL STRUCTURE] AT AC-EXTERNAL GROUND POWER SERVICE PANEL. BOX AT AC-EXTERNAL GROUND POWER SERVICE PANEL(122DR) WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01.
Part: INTERCOSTAL — CORRODED (BS 280-310) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON STRINGER 25RH IN STA. FS= 280 TO FS= 310 AT MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON THE FLOOR SUPPORT BS 349 TO 366 BETWEEN RBL 41 TO RBL 46. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-42-06. AND CRJ-900 SRM 51-42-13.
Part: INTERCOSTAL — CORRODED (BS 310-319) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON INTERCOSTALS BTW FS 310 TO FS 319 STRG 20R AT MAIN AVIONICS COMPARTMENT. (E/E)(SM)(TSI 53-20-304). DUE TO CORROSION LEVEL 2 ON INTERCOSTAL BTW FS310/319 AND STRG 20R AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 581-691) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
INITIAL INSPECTION. CORROSION ON FLOOR SEAT RAIL LBL9, FS 581-661+32, 661+32 -691. (TCI 53-20-245). SEAT RAILS LBL9, FS 581-661+32, 661+32 -691.WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07) .
Part: STRINGER — CORRODED (BS 501-565) · airframe 27,451 hrs · 18,199 cycles
INITIAL INSPECTION: CORROSION ON STRG 26R BTW FS 501 TO 565 AT FWD BAGGAGE BAY. CORROSION ON STRG 26R BTW FS 501/565 AT FWD BAGGAGE BAY WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 PAR. 5, BLENDED AREAS WERE MEASURED AND FOUND WITHIN LIMITS PER CRJ-900 SRM 53-31-03-101-003-A04. EQUIPMENT: DIAL INDICATOR, P/N: 543-783, DUE DATE: 23/APR/20.
Part: DOUBLER — CORRODED (BS 295-310) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON INTERNAL DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. A NEW INTERNAL DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS INSTALLED PER CRJ 900 SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED (BS 333-349) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
INITIAL INSPECTION: CORROSION ON STRINGER 26RH IN STA. FS= 333 TO FS=349 AT MAIN AVIONICS COMPARTMENT. THE STRINGER WAS REPLACED FOR A NEW ONE PER CRJ 900 SRM 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON INTERCOSTALS BTW FS 349 TO FS 364 STRG 20R AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL BTW FS 349 TO FS 364 ON STRINGER 20RH WAS REPLACED PER CRJ-900 SRM 51-42-06. AND CRJ-900 SRM 51-42-21.
Part: FLOOR SUPPORT — CORRODED (BS 1047-1088) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON LH FLOOR SUPPORT SILL IN STA. FS= 1047 TO FS= 1088 AT BAGGAGE BAY. CORROSION ON LH FLOOR SUPPORT SILL BTW FS 1047-1088 AT BAGGAGE BAY WAS REMOVED PER CRJ-900 SRM 53-00-45-201-001-A01 PAR. 6B. AREA WAS MEASURED AND FOUND WITHIN LIMITS PER CRJ-900 SRM 53-00-45-201-001-A01 PAR. 6B, TABLE 3.
Part: ANGLE — CRACKED (BS 280) · airframe 27,451 hrs · 18,199 cycles
AWR IN REF EO R53581 STEP 33, DURING ANGLE RBL9 REMOVAL ON CROSS BEAM FS280 IT WAS FOUND CRACKED. ANGLE RBL 9 FS 280 WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 349-409) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON FLOOR SEAT RAIL BS 349 TO 409, RBL 9. THE SEAT TRACK WAS REPLACED PER AMM 53-00-49-400-801-A01-A07.
Part: CROSSBEAM — CRACKED (BS 280) · airframe 27,451 hrs · 18,199 cycles
AWR IN REF EO R53581 STEP 21 DURING REMOVAL OF LH DRIP TRAY CRACK WAS FOUND ON CROSS BEAM FS 280 LBL13. CROSS BEAM FS 280 LH SIDE WAS REPLACED PER CRJ-900 SRM 51-42-06. AND CRJ-900 SRM 51-42-21.
Part: SEAT TRACK — CORRODED (BS 670-986) · airframe 27,451 hrs · 18,199 cycles
INITIAL INSPECTION. CORROSION ON SIDE SEAT RAILS STGR 15LH, FS 670-722, 743-763, 785-847+14, 847+14-907, 907-986. SIDE SEAT RAILS STGR 15LH, FS 670-722, 743-763, 785-847+14, 847+14-907, 907-986 WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONF. A07).
Part: SEAT TRACK — CORRODED (BS 670-986) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
INITIAL INSPECTION. CORROSION ON SIDE SEAT RAILS STGR 15RH FS 670-722, 743-763, 785-847+14, 847+14-907, 907-986. (TCI 53-20-318) SIDE SEAT RAILS STGR 15RH FS 670-722, 743-763, 785-847+14, 847+14-907, 907-986. WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONF. A07).
Part: SEAT TRACK — CORRODED (BS 847-977) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON FLOOR SEAT RAILS LBL9/RBL9, FS 847+51-977. (TCI 53-20-325) SEAT RAILS LBL9/RBL9, FS 847+51 -977 WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07).
Part: SEAT TRACK — CORRODED (BS 483-581) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON FLOOR SEAT RAIL LBL27, FS 483-581. (TCI 53-20-245). FLOOR SEAT RAILS LBL27, FS 483-581WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07).
Part: SEAT TRACK — CORRODED (BS 379-672) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON SIDE SEAT RAILS STRG15RH FS 379-483, 483-573, 573-661+14, 661+14-672. SIDE SEAT RAILS STRG15RH FS 379-483, 483-573, 573-661+14, 661+14-672. WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07),
Part: SEAT TRACK — CORRODED (BS 379-672) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON SIDE SEAT RAILS STRG15LH FS 379-483, 483-573, 573-661+14, 661+14-672. SIDE SEAT RAILS STRG15LH FS379/483, 483/573, 573/661+14 AND 661+14/672 WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07),
Part: ANGLE — CRACKED (BS 280) · airframe 27,451 hrs · 18,199 cycles
DURING REMOVAL OF LH CROSS BEAM FS 280, CRACK ON LH ANGLE CAP WAS FOUND. CAP ANGLE LH FS 280 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01AND SRM 51-42-13-001-001-A01
Part: SEAT TRACK — CORRODED (BS 691-847) · airframe 27,451 hrs · 18,199 cycles
INITIAL INSPECTION. CORROSION ON FLOOR SEAT RAILS LBL9/RBL9, FS 691-836, 836-847+51. SIDE SEAT RAILS STRGLBL9/RBL9, FS 691-836, 836-847+51. WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801(CONFIG A07), (LEVEL CORROSION 2).
Part: SEAT TRACK — CORRODED (BS 364-691) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON FLOOR SEAT RAIL RBL9, FS 364-485, 485-581, 581-661+32, 661+32 -691. (TCI 53-20-245). FLOOR SEAT RAIL RBL9, FS364/485, 485/581, 581/661+32 AND 661+32/691 WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07),
Part: ACCESS PANEL — CORRODED (PAX DOOR) · airframe 27,451 hrs · 18,199 cycles
CORRSION ON ACCESS PANEL 832DL ON THE PASSENGER DOOR. CORROSION ON THE ACCESS PANEL WAS REMOVED IAW SRM 51-21-06-001-001-A01 PAR. 1 TO 5.B. (1) AND REWORKED AREA WAS MEASURED AS FOLLOW 832DL ORIGINAL THICKNESS: .050"" AND REMAINING THICKNESS: .044"" THEREFORE IT IS WITHIN OF LIMITS PER CRJ 900 S.R.M. 52-11-32-101-001-A01 TABLE 1.
Part: SEAT TRACK — CORRODED (BGS 364-483) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
INITIAL INSPECTION. CORROSION ON FLOOR SEAT RAIL LBL27, FS 364-483. (TCI 53-20-243). SIDE SEAT RAILS LBL27, FS 364-483. WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A07).
Part: COVER — CORRODED (SERVICE DOOR) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON PLATE COVER (PROTECTOR PLATE) OF SERVICE DOOR . CORROSION ON PLATE COVER (PROTECTOR PLATE) WAS REMOVED PER SRM 51-21-06-001-001-A01 PAR. 1 TO 5.B. (1) AND REWORKED AND FOUND WITHIN OF LIMITS PER SRM 52-00-01-101-001-A01, PAR 4.
Part: PANEL — CORRODED (DOOR STAIR) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON FWD/AFT STAIRS SIDE PANEL BELOW LOWER HANDRAILS SUPPORT AT PASSENGER DOOR. CORROSION ON FWD/AFT STAIRS SIDE PANEL BELOW LOWER HANDRAILS SUPPORT AT PASSENGER DOOR WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 PAR. 5. B AND REWORKED AREA WAS MEASURED AS FOLLOW O.T.=0 .032"" AND R.T.= 0.028"" THEREFORE IT IS WITHIN OF LIMITS PER CRJ-900 S.R.M. 52-11-04-101-001-A01 PAR.5A TABLE 1.
Part: SKIN — CORRODED (PAX DOOR) · airframe 27,451 hrs · 18,199 cycles
SEVERAL CORROSION ON EXTERNAL AND INTERNAL INNER SKIN OF PASSENGER DOOR, ON SENTTLEMENT AREAS OF ACCESS PANELS. CORROSION ON EXTERNAL AND INTERNAL INNER SKIN OF PASSENGER DOOR, ON SENTTLEMENT AREAS OF ACCESS PANELS WERE REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 PAR. 5. B AND REWORKED AREA WAS MEASURED AS FOLLOW O.T.=0 .040" AND R.T.= 0.034" THEREFORE IT IS WITHIN OF LIMITS PER CRJ-900 S.R.M. 52-00-01 101-001-A01 PAR.4.A.
Part: PANEL — CORRODED (DOOR STAIR) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON FWD STAIRS PANEL SIDE UPPER EDGE. . CORROSION ON FWD STAIRS PANEL SIDE UPPER EDGE WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 PAR. 5. B AND REWORKED AREA AS FOLLOW O.T.=0 .032" AND R.T.= 0.027" THEREFORE IT IS WITHIN OF LIMITS PER CRJ-900 S.R.M. 52-11-04-101-001-A01 PAR.5A TABLE 1.
Part: SEAT TRACK — CORRODED (BS 375-409) · corrosion level 2 · airframe 27,451 hrs · 18,199 cycles
CORROSION ON FLOOR SEAT TRACK BS 375 TO 409, LBL 9. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49-400-801-A07.
Part: SPRING — CORRODED (DOOR RAIL) · airframe 27,451 hrs · 18,199 cycles
CRACKED FWD/AFT SPRING CLIPS ON HANDRAILS STOWAGE BRACKET AT PASSENGER DOOR. FWD/AFT SPRING CLIPS ON HANDRAILS WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-0A1.
Part: SKIN — CORRODED (PAX DOOR) · airframe 27,451 hrs · 18,199 cycles
INITIAL INSPECTION: CORROSION ON INNER SKIN AT INTERCOSTAL DD2 OF PASSENGER DOOR . CORROSION ON INNER SKIN AT INTERCOSTAL DD2 OF PASSENGER DOOR WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 PAR. 5. B AND REWORKED AREA WAS MEASURED AS FOLLOW O.T.=0 .040" AND R.T.= 0.033" THEREFORE IT IS WITHIN OF LIMITS PER CRJ-900 S.R.M. 52-00-01-101-001-A01 PAR.4.A .
Part: SUPPORT ANGLE — CORRODED (PAX DOOR) · airframe 27,451 hrs · 18,199 cycles
CORROSION ON FWD ANGLE SUPPORT OF PASSENGER DOOR BTW INTERCOSTALS DD5 AND DD6. CORROSION ON FWD ANGLE SUPPORT OF PASSENGER DOOR BTW INTERCOSTALS DD5 AND DD6. WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 PAR. 5. B AND REWORKED AREA WAS MEASURED AS FOLLOW O.T.=0 .063" AND R.T.= 0.059" THEREFORE IT IS WITHIN OF LIMITS PER CRJ-900 S.R.M. 52-00-01-101-001-A01 PAR.4A.
2018
Part: COMPRESSOR — DIRTY (LT ENGINE) · airframe 25,422 hrs · 16,692 cycles
HAD SMOKE IN THE COCKPIT ON TAKE-OFF ROLL, AT 110KTS, ABORTED TAKE-OFF ALSO SMOKE IN AFT OF CABIN REPORTED BY FLT ATTENDANTS NO BRAKE OVERHEAT, AT 1 AND 2 WHEN STOPPED. THRUST REVERSERS DEPLOYED AT APPROX 50% N1 COMPLETED TS 00737, NO BRAKE OVERTEMP/ OR FUSE PLUGS BLOWN. REV INSP NOT REQ PER AD 20-11-17-12. COMPLETED INSP IAW AMM 05-51-27 1C PROCEDURES PART 1 PG 612 NO DEFECTS NOTED, NO FUSE PLUGS MELTED. FOLLOWED FIM 21-22-00, WATER RINSED, IDLE & HIGH PWR BLEED DRY OUT CKS GOOD IAW AMM 72-00-00-100-801. SEE 409 626118 FOR DETAILS. ( LT ENG COMPRESSOR RINSE) EMERGENCY WAS DECLARED AND FIRE TRUCK WAS DISPATCHED TO AIRCRAFT.
Part: LIGHT — MISSING (CABIN) · airframe 25,312 hrs · 16,615 cycles
LUMINESCENT STRIP ON FLOOR MISSING AT SEAT 13B. INSTALLED A SERVICABLE LUMINESCENT STRIP IAW AMM 25-25-01.
Part: LIGHT — DEGRADED (CABIN) · airframe 25,122 hrs · 16,475 cycles
ROWS 13 DC FWD ILLUMINESCENT TRACK DEGRADED. INSTALLED FILTER FILM ON EXIT ROW 13 CD ILLUMINESCENT TRACK IAW CMM 33-57-07.
Part: LIGHT — MISSING (CABIN) · airframe 25,102 hrs · 16,457 cycles
EMERGENCY LIGHT STRIP MISSING AT 13CD. INSTALLED EMERGENCY LIGHT STRIP AT 13CD IAW AMM 33-51-01. ALL CHECKS GOOD.
Part: LIGHT — MISSING (SEAT ROW 12DC) · airframe 24,153 hrs · 15,774 cycles
EXIT ROW MISSING PIECE OF EMERGENCY LIGHT SEAT 12DC. REPLACED THE SECTION OF EMERGENCY LIGHT IAW CMM 31-55-07, AND AMM 33-51-01.
Part: OXYGEN MASK — UNWANTED DEPLOY (FWD LAVATORY) · airframe 24,089 hrs · 15,726 cycles
FWD LAVATORY OXYGEN MASK DEPLOYED DURING CRUISE. NO OTHER MASKS DEPLOYED. STOWED THE FWD LAVATORY OXYGEN MASK IAW AMM 35-11-15, OK FOR SERVICE.
Part: OXYGEN BOTTLE — LOW PRESSURE (PAX) · airframe 24,047 hrs · 15,695 cycles
FORWARD PAX OXYGEN BOTTLE HAD LOW PRESSURE. REMOVED AND REPLACED THE FORWARD PASSENGER OXYGEN BOTTLE IAW AMM 35-31-01.
Part: KNOB — BROKEN (MEGAPHONE) · airframe 23,617 hrs · 15,413 cycles
MEGAPHONE IN AFT OVERHEAD VOLUME KNOB BROKEN. R & R THE MEGAPHONE IAW AMM 25-61-14, OPS CHECKED GOOD.
2017
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,456 hrs · 15,668 cycles
FLASHLIGHT BEHIND CAPTAIN`S SEAT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT POWER UNIT IAW CMM 25-60-11. NO FURTHER DEFECTS NOTED.
Part: ESCAPE ROPE — DETACHED · airframe 21,837 hrs · 14,160 cycles
DURING PREFLIGHT, FOUND CREW ESCAPE ROPE DETACHED. ATTACHED THE CREW ESCAPE ROPE IAW AMM 25-63-01. AIRCRAFT OK FOR SERVICE.
Part: PAD — CORRODED (BS 565) · airframe 21,771 hrs · 14,109 cycles
CARGO PAD AT BS 565, STRINGER 26R HAS CORROSION. REMOVED AND REPLACED THE CARGO PAD IAW SRM 51-42-21.
Part: SEAT TRACK — CORRODED (BS 846-977) · airframe 21,771 hrs · 14,109 cycles
LEFT AISLE SEAT TRACK HAS CORROSION BETWEEN BS 846+62 AND 977, IN CABIN. OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-074, 670-53-00-343 AND AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 846-977) · airframe 21,771 hrs · 14,109 cycles
LEFT AISLE SEAT TRACK HAS CORROSION BETWEEN BS 846+62 AND 977, IN CABIN. REMOVED AND REPLACED THE SEAT TRACK IAW REO 670-53-00-074, 670-53-00-343 AND AMM 53-00-49-400-801.
Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 21,771 hrs · 14,109 cycles
STRINGER SPLICE 26R HAS CORROSION JUST FWD OF FRAME BS 333, IN THE FWD E & E BAY. REMOVED AND REPLACED THE STRINGER SPLICER IAW SRM 51-42-06 AND 51-42-21.
Part: STRINGER SPLICE — CORRODED (BS 328-338) · airframe 21,771 hrs · 14,109 cycles
STRINGER SPLICE 25R BS 328 - 338 CORRODED. REMOVED AND REPLACED THE STRINGER SPLICE IAW SRM 51-42-06, & 51-42-21.
Part: SEAT TRACK — CORRODED (BS 846) · airframe 21,771 hrs · 14,109 cycles
RIGHT AISLE SEAT TRACK HAS CORROSION BETWEEN BS 830.40 AND 846+62, IN CABIN. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (BS 846-977) · airframe 21,771 hrs · 14,109 cycles
RIGHT AISLE SEAT TRACK HAS CORROSION BETWEEN BS 846+62 AND 977, IN CABIN. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (BS 830-846) · airframe 21,771 hrs · 14,109 cycles
LEFT AISLE SEAT TRACK HAS CORROSION BETWEEN BS 830.40 AND 846+62, IN CABIN. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.
Part: DEFIBRILLATOR — NO TEST (CABIN) · airframe 21,498 hrs · 13,908 cycles
AED NOT DISPALYING; OK STATUS WHEN TESTED. R&R AED IN REF TO AMM 25-60-00 S/N OFF/ON NSN P/N ON/OFF 3011790-001129. "
Part: OXYGEN BOTTLE — BROKEN · airframe 21,170 hrs · 13,686 cycles
TABS TO HOLD HOSE ON PORTABLE OXYGEN BOTTLE BROKE. REMOVED AND REPLACED OXYGEN MASK ON PASSENGER PORTABLE OXYGEN BOTTLE IAW TECHNICAL SUPPLEMENT TS 000755-2013.
2016
Part: LIGHT — MISSING (CABIN) · airframe 20,283 hrs · 13,078 cycles
DURING PREFLIGHT, F/A NOTED ROW 12CD FLOOR EMERGENCY LIGHT MISSING. INSTALLED THE EMERGENCY LIGHT ON 1A IAW AMM 33-51-01.
Part: LIGHT — BROKEN (CABIN) · airframe 20,163 hrs · 13,002 cycles
FA ADVISES THAT A SMALL PORTION OF EMERGENCY LIGHT STRIP IS BROKEN NEAR GALLEY & FWD LAV. R & R THE EMERGENCY LIGHT IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED.
Part: HOSE — DISCONNECTED (OXYGEN MASK) · airframe 19,938 hrs · 12,826 cycles
FIRST OFFICERS OXYGEN MASK HEAD STRAP AIR HOSE IS DISCONNECTED FROM UNIT ON MASK, RENDERING MASK INOPERATIVE. SWAPPED 02 MASK WITH OBSERVER'S 02 MASK. DEFERRED OBSERVER'S MASK IAW MEL 35-10-1. ENTERED IN MM02. PLACARD INSTALLED. MAINTENANCE NOTIFIED. R & R THE OBSERVERS OXYGEN MASK IAW AMM 35-11-12. PERFORMED AN OPS TEST OF THE CREW MASK MIC IAW AMM TASK 23-51-00-710-801. ALSO, PERFORMED A LEAKAGE TEST IAW TASK 35-10-00-790-801. PERFORMED OPS TEST OF CREW OXYGEN SYSTEM IAW TASK 35-10-00. NO LEAKS FOUND. OPS CHECKS ARE GOOD. MM02 UPDATED. PLACARD REMOVED.
Part: CHARGER — FAULTY (CABIN) · airframe 19,687 hrs · 12,637 cycles
MAIN CABIN PAX DOOR EMER EXIT LIGHT INOPERATIVE. FOUND BATTERY PACK 1 CHARGER AT FAULT. REPLACED CHARGER WITH SERVICEABLE ASSEMBLY. REPLACED BATTERY PACK 1. EMER LIGHT SYS CHECKED GOOD. WORK DONE IAW AMM 33-51-17-400-801 & 33-51-17-400-802.
Part: SIGN — DAMAGED (CABIN) · airframe 19,687 hrs · 12,637 cycles
PASSENGER DOOR LOWER EMER EXIT SIGN ASSEMBLY DAMAGED. NEEDS REPLACED. R & R EMER EXIT SIGN DS156 IAW AMM 33-51-05. OPERATIONS CHECKED GOOD. OK FOR SERVICE.
Part: FIRE BOTTLE — UNSERVICEABLE (CABIN) · airframe 19,612 hrs · 12,584 cycles
WATER FIRE EXTINGUISHER OPEN, WIRE BROKEN. R & R WATER FIRE EXTINGUISHER IAW AMM 26-23-01. OPERATIONS CHECKED GOOD.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
IN AFT CARGO COMPARTMENT BELOW FLOOR, BETWEEN FS 1031.00 - 1047.00, STRINGER 26R HAS PITTING CORROSION. REMOVED DAMAGED AREA & REPAIRED IAW EA CRJ9 53-04245. REPLACED DAMAGED SECTION OF STRINGER.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
IN AFT CARGO COMPARTMENT BELOW FLOOR, BETWEEN FS 985.00 - 1000.00, STRINGER 26R HAS PITTING CORROSION. CONTINUATION CARD 81518311 OP 186. R & R DAMAGED SECTION IAW EA CRJ953-04245.
Part: FRAME — CRACKED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
FRAME AT FS 1031 RT STRINGER 26 FOUND CRACKED. REPAIRED FRAME IAW EA CRJ953-04307 REV IR.
Part: FRAME — CRACKED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
FRAME AT FS 1015, STRINGER RT 26 FOUND CRACKED. REPAIRED FRAME IAW SRM 53-00-06-201-001-A03.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
CORROSION ON OTBD SEAT RAILS LT & RT, BETWEEN FS 669.40 - 977.00 AT VARIOUS LOCATIONS. CONTINUATION OF MWC JOB 81518311 OP 151. CONTINUATION CARD 81518311 OPS 111, 133, 140, 147 & 151. R & R CORRODED SEAT RAIL SECTIONS OTBD LT & RT SIDES FS 699.4 - 977.0 IAW AMM 53-00-49-400-801-A07, REO 670-53-00-343 & SRM 51-40-11-001-001-A01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
CORROSION ON OTBD SEAT RAILS LT & RT, BETWEEN FS 379.00 - 669.40, AT VARIOUS LOCATIONS. CONTINUATION FROM JOB 81518311 CO 15183116 OP 112. CONTINUATION CARD 81518311 OPS 112 & 164. REPAIRED OR R & R SEAT RAILS, BETWEEN FS 379.0 & FS 669.4 LT & RT SIDE AS REQUIRED TO REMOVE CORROSION IAW SRM 53-31-49-101-001-A02, AMM 53-00-49-400-801-A07 & REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
CORROSION ON OTBD SEAT RAILS LT & RT, BETWEEN FS 669.40 - 977.00 AT VARIOUS LOCATIONS. CONTINUATION FROM JOB 81518311 CO 15183116 OP 111. CONTINUATION CARD 81518311 OPS 111, 140, 147, 151, & 165. R & R CORRODED SEAT RAIL SECTIONS OT LT & RT SIDES IAW AMM 53-00-49-400-801-A07, REO 670-53-00-343 & SRM 51-40-11-001-001-A01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
CONTINUATION CORROSION ON OTBD SEAT RAILS LT & RT, BETWEEN FS 669.40 - 977.00 AT VARIOUS LOCATIONS. CONTINUATION FROM JOB 81518311 CO 15183116 OP 147. CONTINUATION CARD 81518311 OPS 111, 133, 140, 147, & 165. R & R CORRODED SEAT RAIL SECTIONS OTBD LT & RT SIDES FS 699.4 - 977 IAW AMM 53-00-49-400-801-A07, REO 670-53-00-343 & SRM 51-40-11-001-001-A01.
Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
LEFT & RIGHT FS 280 BEAMS CRACKED. R & R LT & RT FS 280 CROSSBEAMS IAW SRM 51-42-06-001- 001-A01, 51-42-21-001-001-A01 & 51-42-22-001-001-A01. THIS IS A MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
CORROSION ON OTBD SEAT RAILS LT & RT, BETWEEN FS 669.40 - 977.00 AT VARIOUS LOCATIONS. CONTINUATION OF MWC 133. CONTINUATION FROM JOB 81518311 CO 15183116 OP 111 & 133. CONTINUATION CARD 81518311 OPS 111, 133, 147, 151, & 165. R & R CORRODED SEAT RAIL SECTIONS OTBD LT & RT SIDES FS 699.4 - 977.0 IAW AMM 53-00-49-400-801-A07, REO 670-53-00-343 & SRM 51-40-11-001-001-A01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
CORROSION ON OTBD SEAT RAILS LT & RT, BETWEEN FS 379.00 - 669.40 AT VARIOUS LOCATIONS. CONTINUATION CARD 81518311 OPS 146 & 164. REPAIRED, R & R SEAT RAILS, AS REQUIRED TO REMOVE CORROSION IAW SRM 53-31-49-101-001-A02, AMM 53-00-49-400-801-A07 & REO 670-53-00-343.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
CORROSION ON CTR SEAT RAILS LT & RT, BETWEEN FS 477.40 - 669.40 AT VARIOUS LOCATIONS. CONTINUATION CARD 81518311 OPS 127 & 156. REPAIRED CORROSION ON SEAT RAILS IAW SRM 53-31-49-101-001-A02, & REPLACED OUT OF LIMITS SEAT RAIL IAW REO 670-53-00-343 & AMM 53-00-01-801-A07 AT VARIOUS LOCATIONS OF CTR SEAT RAILS.
Part: SEAL — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
SERVICE DOOR SURROUND STRUCTURE, STRIKER SEAL CORRODED AROUND FASTENER HOLES, BETWEEN FS 320.68 - FS 348.02. DRILLED SERVICEABLE STRIKER SEAL, INSTALLED SEAL & INSTALLED SERVICEABLE KICK PLATE AMM 53-21-23-400-801-A01, SRM 51-40-11-001-001-A01 & 51 -42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
CORROSION ON OTBD SEAT RAILS LT & RT, BETWEEN FS 669.40 - 977.00 AT VARIOUS LOCATIONS. CONTINUATION CARD 81518311 OPS 133, 140, 147, 151, & 165. R & R CORRODED SEAT RAIL SECTIONS OTBD LT & RT SIDES IAW AMM 53-00-49-400-801-A07, REO 670-53-00-343 & SRM 51-40-11-001-001-A01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
CORROSION ON OTBD SEAT RAIL LT & RT, BETWEEN FS 669.40 - 977.00 AT VARIOUS LOCATIONS. CONTINUATION FROM JOB 81518311 CO 15183116 OP 140. CONTINUATION CARD 81518311 OPS 111, 133, 140, 151, & 165. R & R CORRODED SEAT RAIL SECTIONS OTBD LT & RT SIDES FS 699.4 - 977.0 IAW AMM 53-00-49-400-801-A07 & REO 670-53-00-343 & SRM 51-40-11-001-001-A01.
Part: HOUSING — DAMAGED (E&E DOOR) · airframe 19,540 hrs · 12,528 cycles
FOUND MAIN AVIONICS DOOR HANDLE HOUSING HAS MULTIPLE INDICATIONS NOTED AROUND HOUSING RADIUS 80% FSH. FAILED NDT INSPECTION. REMOVED MAIN AVIONICS DOOR, R & R MAIN AVIONICS DOOR HANDLE. PAINTED AREA & INSTALLED MAIN AVIONICS DOOR. OPERATIONS CHECKED AVIONICS DO OR AMM USED 52-42-00-400-801 A01, 52-43-03-400-801 A01, SRM 51-42-42-001-001-A01, 51-25-01-001-001-A01 & 52-42-00-710-801 A01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
CORROSION ON OTBD SEAT RAILS LT & RT, BETWEEN FS 379.00 - 669.40 AT VARIOUS LOCATIONS. CONTINUATION OF MWC JOB 81518311 OP 146. CONTINUATION CARD 81518311 OPS 112 & 146. R & R SEAT RAILS AS REQUIRED TO REMOVE CORROSION IAW SRM 53-31-49-101-001-A02, AMM 53-00-49-400-801-A07 & REO 670-53-00-343.
Part: ANGLE — CORRODED (PAX DOOR) · airframe 19,540 hrs · 12,528 cycles
PASSENGER DOOR KICK PLATE ANGLE HAS CORROSION AT FWD & AFT ENDS. CONTINUATION CARD 81518311 OP 56. R & R KICK PLATE ANGLE IAW SRM 51-40-11, 51-42-21-001-001-A01 & 51-42-06-001-001-A0 1.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
CORROSION ON LT SIDE SEAT RAIL, BETWEEN FS 565 - 677 AT VARIOUS LOCATIONS. CONTINUATION CARD 81518311 OP 163. R & R CORRODED SEAT TRACK SECTIONS OF LT SIDE SEAT RAIL, BETWEEN FS 565 & 677 IAW REO 670-53-00-343 & AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
CONTINUATION OF MWC JOB 81518311 OP 148. CORROSION ON LT SIDE SEAT RAIL, BETWEEN FS 565 - 677 AT VARIOUS LOCATIONS. R & R CORRODED SEAT TRACK SECTIONS OF LT SIDE SEAT RAIL, BETWEEN FS 565 & 677 IAW REO 670-53-00-343 & AMM 53-00-49-400-801-A07.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,582 cycles
FS 280 AT COCKPIT THRESHOLD, FWD J ANGLE & SACRIFICIAL STRIP IS CORRODED. R & R J ANGLE AT FS 280 IAW SRM 51-42-06-001-001-A01 & 57-42-21-001-001-A01. SACRIFICIAL STRIP FOUND TO BE SERVICEABLE.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
CORROSION ON OTBD SEAT RAILS LT & RT, BETWEEN FS 379.00 - 669.40 AT VARIOUS LOCATIONS. REPLACED CORRODED OTBD SEAT RAILS VARIOUS LOCATIONS IAW SRM 53-31-49-101-001-A02 & REO 670-53-00-343 REV M DATED 2015 10 19.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 19,540 hrs · 12,528 cycles
FS 280 LT & RT BULKHEAD WEBS CORRODED. REPAIRED LT & RT FS 280 BULKHEAD WEBS IAW REO 670-53-11-594 REV A DATED 06 26 15.
2015
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,699 hrs · 11,997 cycles
CAPTAINS SIDE EMER FLASHLIGHT DOES NOT BLINK RED LIGHT. REPLACED FLASHLIGHT BATTERY AS REQUIRED IAW AMM 25-61-00. OPERATIONS TESTED GOOD.
Part: OXYGEN BOTTLE — LOW (CABIN) · airframe 18,333 hrs · 11,759 cycles
AFT EMER O2 BOTTLE NEEDS TO BE SERVICED, O2 LEVEL AT OR BELOW MINIMUM LEVEL. SERVICED AFT PORTABLE O2 CYLINDER TS 000432-2013.
Part: LIGHT — BROKEN (CABIN) · airframe 18,224 hrs · 11,682 cycles
FLOOR TRACK LIGHTING AT 13C BROKEN. SECURED FLOOR TRACK LIGHTING AT 13C IAW AMM 33-51-1.
Part: LIGHT — DETACHED (CABIN) · airframe 18,214 hrs · 11,675 cycles
GALLEY EMER LIGHTING STRIP IS DETACHED. RE-INSTALLED GALLEY EMER FLOOR PATH LIGHTING IAW 33-51-01.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,114 hrs · 11,616 cycles
EMERGENCY FLOOR LIGHTING STRIP MISSING IN FRONT 13CD. INSTALLED NEW EMER FLOOR LIGHTING STRIP IN FRONT OF 13CD IAW AMM 33-51-01.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,107 hrs · 11,612 cycles
FIRST OFFICERS EMER FLASHLIGHT RED LED INDICATOR NOT BLINKING. REPLACED BATTERY IN FIRST OFFICERS EMER FLASHLIGHT. OPERATIONS CHECKED GOOD. PN P4-01-0021.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 18,107 hrs · 11,612 cycles
FIRST OFFICERS EMER FLASHLIGHT RED LED INDICATOR NOT BLINKING. REPLACED BATTERY IN FIRST OFFICERS EMER FLASHLIGHT. OPERATIONS CHECKED GOOD. PN P4-01-0021.
Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 17,840 hrs · 11,419 cycles
FLIGHT ATTENDANT LIFE VEST BAG TORN. R & R LIFE VEST IAW AMM 25-61-03.
Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 17,744 hrs · 11,347 cycles
AT CRUISE ALTITUDE JUST PRIOR TO TOD HYD 3 LO PRESS CAUTION MSG DISPLAYED. ASSOCIATED INBD GND SPLRS MSG DISPLAYED. RAN POM PROCEDURE, UNABLE TO ESTABLISH SYS 3 PRESS. PERFORMED ALTERNATE LG EXTENSION. REF PILOT WRITE UP AML PG 3197921-1 3A CB POPPED IN FLIGHT. R & R 3B HYD PUMP PRESS SWITCH IAW AMM 29-34-01, PN OFF & ON 967008-1, SN OFF 5004, SN ON HYD 9724. OPERATIONS CHECKED GOOD. R & R 3A HYD PUMP IAW AMM 29-12-03, PN OFF & ON 66195-01, SN OFF K1925, SN ON K2959. OPERATIONS CHECKED FAILED. REF AML PG 3197923-1 FOR EL OF 3A HYD PUMP. IN FLIGHT 3A HYD PUMP CB POPPED IN AVIONICS BAY. RESET ALT EXTENSION HANDLE IAW 05-51-31. DEFER 3A HYD PUMP IAW MEL 29-12-1, PLACARD INSTALLED & MM02 UPDATED. REF DISC NR 2 FOR CAT II DEFERRAL. EMER WAS DECLARED.
Part: LIGHT — UNSECURE (CABIN) · airframe 17,354 hrs · 11,049 cycles
A TWO FOOT SECTION OF EMER LIGHTING FLOOR STRIP IN FRONT OF THE BEVERAGE CARTS NEEDS TO BE SECURED. SECURED EMER FLOOR TRACK STRIP IN GALLEY AREA IAW AMM 33-51-00. GOOD FOR SERVICE.
Part: LIGHT — LOOSE (CABIN) · airframe 16,972 hrs · 10,785 cycles
EMERGENCY EXIT STRIP ROW 13C CAME LOOSE & WILL NOT STAY ATTACHED. SECURED EMER EXIT FLOOR STRIP AT 13C IAW AMM 25-20-01. OK FOR SERVICE.
Part: LIGHT — MISSING (CABIN) · airframe 16,818 hrs · 10,687 cycles
FLOOR LEVEL EMER EXIT LIGHTING STRIP IS MISSING IN THE GALLEY. INSTALLED RT FWD MOST EMER FLOOR PATH LIGHT, FILTER FILM & COVER IAW AMM 33-51-01. ACFT OK FOR CONTINUED SERVICE, PNS PL88-900LH00, PL88910LH00 & PL88930LH05.
2014
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,477 hrs · 10,465 cycles
EMERGENCY LIGHTS, HAS ONE BULB INOPERATIVE. REPLACED THE BULB IAW AMM 33-26-01.
Part: PIN — MISSING (EMERGENCY LIGHTS) · airframe 14,826 hrs · 9,369 cycles
LEFT FWD EMERGENCY LIGHT WIRING IS MISSING 2 PINS & THE LT AFT EMERGENCY LIGHT WIRING IS MISSING 1 PIN. REPLACED 2 PINS ON LT FWD EMERGENCY LIGHT WIRING & 1 PIN ON LT AFT EMERGENCY LIGHT WIRING IAW CRJ 900 ESPM 20-16-05. OPERATIONS CHECKED GOOD IAW CRJ 700 900 AMM 33-51-00-710-801-A01.
Part: PANEL — CHAFED (RT WING) · airframe 14,830 hrs · 9,370 cycles
RIGHT WING FLAP LE PANEL 684EB HAS SEVERE CHAFING. DRILLED & COUNTER SUNK NEW LE PANEL IAW SRM 51-54-02-001-001-A01.
Part: SEAT TRACK — UNKNOWN (FUSELAGE) · airframe 14,830 hrs · 9,370 cycles
THE FIRST THREE EACH SEAT TRACKS FROM LT TO RT, AFT OF PAX & SERVICE. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A07 TOOL CVT306-3 1-8-15.
Part: PANEL — CHAFED (RT WING) · airframe 14,830 hrs · 9,370 cycles
CHAFING ON RT WING PANEL 84ET DOWN TO BARE METAL. PANEL OUT OF LIMITS IAW SRM 57-52-01-101-001-A01. LOCATED & DRILLED NEW PANEL 684ET IAW SRM 51-40-11-001-001-A01. PAINTED PANEL IAW SRM 51-25-01-001-001-A01.
Part: PANEL — DAMAGED (WING) · airframe 14,830 hrs · 9,370 cycles
PANEL 584ET NEEDS REPLACED. R & R PANEL 584ET & NUTPLATE CLIPS IAW THE FOLLOWING SRMS 51-42-06-001-001-A01 & 51-40-11-001-001-A01. DAMAGED OUT OF LIMITS.
2013
Part: POWER UNIT — FAULTY (FLASHLIGHT) · airframe 14,142 hrs · 88,935 cycles
FLASHLIGHT NEXT TO EXTRA FLIGHT ATTENDANT JUMP SEAT IS INOPERATIVE. DEFERRED IAW MX 95765 IAW MEL 25-61-4A. ENTERED INTO MM02 & INSTALLED PLACARD. R & R EXTRA FLIGHT ATTENDANT`S FLASHLIGHT POWER UNIT IAW CMM 25-60-11. OPERATIONS CHECKED GOOD. THIS CLEARS DM 2298322-1, CLEARED FROM MM02 & MX NOTIFIED 4632. PLACARD REMOVED FROM LOF CAN.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 12,589 hrs · 7,944 cycles
AFT FA EMERGENCY FLASHLIGHT NOT CHARGING. DEFERRED AFT FA EMERGENCY FLASHLIGHT PER MEL 25-61-4A AUTH BY MXC. REMOVED AND REPLACED AFT FA EMERGENCY FLASHLIGHT IAW AMM 25-61-02. REMOVED FROM MM02. MXC NOTIFIED. P/N ON/OFF P2-07-0001-214.
Part: NUT — LOOSE (LG DOOR) · airframe 12,051 hrs · 7,598 cycles
UPON GEAR RETRACTION AFTER DEPARTING JFK, WE RECEIVED "GEAR DISAGREE" WARNING MESSAGE FOLLOWED POM PROCEDURE. GEAR INDICATED NORMAL (DOWN AND LOCKED) RETURNED TO JFK FOR A NORMAL LANDING. COMPLIED WITH FCR 32006. RE-TORQUED DOOR BRACKET NUTS PER FCR 23006. GEAR SWINGS DONE IAW 32-30-00. ALL CHECKS GOOD.
2012
Part: BEAM — CRACKED (FUSELAGE) · airframe 11,803 hrs · 7,443 cycles
RBL 12 BEAM CRACKED AT FS 280. REPAIRED CRACKED RBL 12 BEAM IAW EOR53259. P/N CC670-53-11-755-2.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,803 hrs · 7,443 cycles
STGR 25R HAS CORROSION BETWEEN FRAMES 349 AND 333, IN THE FWD E&E BAY. REMOVED AND REPLACED LONGERON AT 25R FRAME 333 TO FRAME 364 IAW CRJ 900 SRM 51-42-06. P/N SH670-32103-4. AAR SM-10.
Part: SKIN — CRACKED (FUSELAGE) · airframe 11,803 hrs · 7,443 cycles
FORWARD EQUIPMENT COMPARTMENT SKIN CRACKED O/B AFT CORNER UNDER ADG HYD PUMP HANDLE. REPAIRED FORWARD EQUIPMENT COMPARTMENT SKIN IAW CRJ 900 REO #670-53-11-509.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 11,803 hrs · 7,443 cycles
STGR 23R HAS CORROSION BETWEEN FRAMES 364 AND 333, IN THE FWD E&E BAY. REMOVED AND REPLACED STGR 23R BETWEEN FRAME 374 AND FS 333 IAW CRJ 900 SRM 51-42-06. P/N SH670-31380-1.
Part: SILL — CORRODED (FUSELAGE) · airframe 11,803 hrs · 7,443 cycles
AFT CARGO DOOR SILL CORRODED AT 15EA SCREW HOLES AND 3 PLACES AT UPPER BAND. REPAIRED AFT CARGO DOOR SILL IAW BOMBER REO# 670-53-61-913.
Part: BEAM — CRACKED (FUSELAGE) · airframe 11,803 hrs · 7,443 cycles
LBL 12 BEAM CRACKED AT FS 280. REPAIRED CRACKED LBL 12 BEAM IAW EOR53259. P/N CC670-53-11-755-1.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 11,803 hrs · 7,443 cycles
STR 26L SPLICE AT FS 333 CORRODED BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED STR 26L SPLICE.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 11,803 hrs · 7,443 cycles
SPLICE AT STGR 25R HAS CORROSION AT FRAME 333, IN THE FWD E&E BAY. REMOVED AND REPLACED SPLICE AT STGR 25R FS 333 IAW CRJ-900 SRM 51-42-06. P/N SH370-32429-3. AAR SM-10.
Part: BEAM — CORRODED (FUSELAGE) · airframe 11,803 hrs · 7,443 cycles
WHILE WORKING DRIPTRAY REPAIR AT RIGHT FS 280 CORROSION ON BEAM. REMOVED AND REPLACED 280 BEAM IAW EO R53261, R53117 AND R53127. P/N CC670-34094-2S.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 11,803 hrs · 7,443 cycles
AFTER REMOVING FLOORBOARD FOR 280 INSPECTION FOUND SERVICE DOOR FLOORBOARD LANDING CORRODED. REMOVED AND REPLACED SERVICE DOOR FLOORBOARD LANDING IAW CRJ 900 SRM 51-42-06 + 51-42-21. P/N SH670-31986-1.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 11,803 hrs · 7,443 cycles
LINE BRACKET CRACKED AT FS 1150 AND STR 9R APPROX AFT EQUIPMENT BAY (246-004). INSTALLED NEW FS 1150 LINE BRACKET IAW CRJ 900 SRM 51-42-21. P/N B0203013-08, HST10AG-5-2, PG6W2-202 AND 2024-T3.040.
Part: FITTING — BROKEN (FUSELAGE) · airframe 11,803 hrs · 7,443 cycles
RIGHT AFT EQUIPMENT BAY HAS A CLIP BROKEN ON THE RIGHT SIDE FS 1155 AND STR 7 (APPROX) 246-002. INSTALLED NEW FS 1155 CLIP IAW CRJ 900 SRM 51-42-21. P/N HST10AG5-2, PG6W2-202, B0203013-08 AND 2024-T3.040.
Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 11,803 hrs · 7,443 cycles
900-52-830-300, PAX DOOR RISER SUPPORT ANGLE IS CRACKED IN THE MIDDLE AFT SIDE. REPAIRED & INSTALLED PAX DOOR RISER SUPPORT ANGLE IN THE MIDDLE AFT SIDE IAW CRJ-900 SRM 52-11-04. P/N PLT214-6-5, CR3243-5-3, AND 601R31772-5S.
Part: BEAM — CORRODED (FUSELAGE) · airframe 11,803 hrs · 7,443 cycles
WHILE WORKING DRIPTRAY REPAIR AT LEFT FS 280 CORROSION FOUND ON BEAM. REMOVED AND REPLACED 280 BEAM IAW EO R53261 AND R53127. P/N CC670-34094-1S.
Part: LIGHT — DAMAGED (CABIN) · airframe 11,564 hrs · 7,291 cycles
EMERGENCY FLOOR TRACK DAMAGED ON RIGHT SIDE OF GALLEY. INSTALLED SERVICEABLE FLOOR TRACK LIGHTING ON RIGHT SIDE OF GALLEY IAW CRJ 900 AMM 33-51-01. NO FURTHER ACTION REQUIRED AT THIS TIME. P/NS INSTALLED PL88-900LH00, PL88-950LH01, & PL88-930LH01.
Part: TAPE — MISSING (SERVICE DOOR) · airframe 10,698 hrs · 6,743 cycles
REFLECTIVE STRIP MISSING ON THE RIGHT SIDE OF THE GALLEY SERVICE DOOR. REPLACED MISSING REFRACTIVE STRIP IN GALLEY IAW STANDARD PRACTICES.
2011
Part: GLOWSTRIP — MISSING (CABIN) · airframe 8,673 hrs · 5,535 cycles
FLOOR GLOWSTRIP IS MISSING IN THE FORWARD GALLEY. INSTALLED SERVICEABLE FLOOR GLOWSTRIP IAW AMM. 33-51.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,336 hrs · 4,710 cycles
EXTERIOR RT AFT EMERGENCY (OVERWING) EXIT DOOR EMERGENCY LIGHT INOPERATIVE. R & R RT AFT EMERGENCY LIGHT ASSY AND REPINNED CONNECTOR IAW AMM 33-51. ALL CHECKED GOOD.
Part: DOOR FRAME — DENTED (FUSELAGE) · airframe 7,280 hrs · 4,677 cycles
DENT ON UPPER RT SIDE MAIN CABIN DOOR FRAME, APPROX 4 INCHES FROM TOP. PERFORMED TEMPORARY REPAIR TYPE II OF DENT ON UPPER RT SIDE MAIN CABIN DOOR FRAME APPROX 4 INCHES FROM TOP IAW REO 670-53-22-011. TEMP REPAIR GOOD FOR 400 FLIGHT HOURS, APPROX 8 MAN HRS TO REPAIR.
2008
Part: A/C PACK — SMOKE
SMOKE WAS SMELLED AND SEEN COMING FROM RT PRESSURIZATION PACK FROM ABOUT THE LAST FIVES ROW OF THE CABIN. COULD NOT DUPLICATE PROBLEM. CHECKED AFT EQUIPMENT BAY FOR LEAKS, NO LEAKS NOTED. (K)