N297PQ
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.
119 reports on file, 2015-03-14 – 2026-08-09.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 28,312 hrs · 21,731 cycles
FWD EXTERIOR EMERGENCY LIGHT DS52 INOPERATIVE. DEFERRING FWD EXTERIOR EMERGENCY LIGHT DS52 IAW MEL 33-51-2A PLACARD INSTALLED MM02. MX PROCEDURES COMPLIED WITH. LIGHT DS52 POPS BATTERY CHARGER FUSE AFTER A FEW SECONDS, NO SHORT FOUND ON LIGHT ASSY. SCHEMATIC SHOWS EXT LIGHT POWERED FROM PS36P1-10, ACFT WIRING SHOWS LIGHT WIRED TO PIN 11. IAW SSM 33-50-00, WM 33-21-03, 25-28-01. REPLACED BATTERY CHARGER IAW AMM 33-51-17. C/W WIRING CHECKS IAW ESPM 20-12-01. FOUND NO VOLTS AT DS52P1 PIN 1. FOUND AN OPEN CIRCUIT BTWN DS52P1 PIN 1 & PS36P1 PIN 10. MEL 4183873-2 REQ'S FURTHER T/S & REMAINS OPEN. FOUND FUSE BLOWN ON PS36 CHARGER, R & R PS36 CHARGER & BATTERY PACK IAW AMM 33-51-17. OPS CK GOOD.
Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 28,309 hrs · 21,729 cycles
EMERGENCY CEILING LIGHTS LT#1 DS429 LT#2 DS431. FOUND FAULTY BATTERY CHARGER ASSEMBLY. R & R NR 2 BATTERY CHARGER PS36 IAW AMM 33-51-17. FWD EMERGENCY LIGHTS DS429 + DS431 FUNCTIONING PROPERLY.
Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 28,294 hrs · 21,717 cycles
RIGHT FWD EMERGENCY LIGHT INOPERATIVE. R & R BATTERY CHARGER 2 IAW AMM 33-51-17. OPS TESTED GOOD.
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 28,281 hrs · 21,709 cycles
FOUND FWD RT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R LIGHT BULB. OPS TEST FAILED. SUSPECT INOPERATIVE HOUSING. NO FIX. DEFERRING RT FWD EMERGENCY LIGHT IAW MEL 33-51-2A. PLACARD INSTALLED. R & R EMERGENCY LIGHT IAW AMM 33-51-15. R & R BATTERY PACK 1 & 2 IAW AMM 33-51-17. R & R BATTERY PACK CHARGER 2 IAW AMM 33-51-17. R & R EMERGENCY LIGHTS RELAY (K198) IAW AMM 33-51-19. ALL CORRECTIVE ACTIONS DID NOT FIX PROBLEM. R & R EMERGENCY LIGHT BATTERY PACK PS36. OPS TESTED GOOD IAW AMM 33-51-17.
Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 28,271 hrs · 21,702 cycles
CEILING EMERGENCY LIGHTS IN 1ST CLASS & EXTERIOR SERVICE DOOR EMERGENCY LIGHT ARE INOP. R/R BATTERY CHARGER 2 IAW CRJ900 AMM 33-51-17 OPC GOOD P/N 11-0049 S/N OFF 26590 ON 23019
Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CRACK ON DOOR POST WAS FOUND. DOOR POST WAS REPAIRED PER CRJ900 SRM 51-71-59-001-001-A01
Part: PANEL — CRACKED (PAX DOOR) · airframe 27,630 hrs · 21,175 cycles
CRACKS (4 LOCATIONS) ON AFT SIDE PANEL AT PASSENGER DOOR. AFT SIDE PANEL AT PASSENGER DOOR WAS REPAIRED PER CRJ-900 SRM 52-11-04-201-004-A01
Part: HANDLE — CRACKED (ZONE 800) · airframe 27,630 hrs · 21,175 cycles
CRACK ON EXTERNAL HANDLE FLAPPER AT PASSENGER DOOR . EXTERNAL HANDLE FLAPPER AT PASSENGER DOOR WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-25-06-001-001-A01, SRM 51-25-16-001-001-A01 AND AMM 20-60-04-400-801-A01.
Part: SUPPORT FITTING — DAMAGED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
ELONGATED HOLE ON FWD LEFT SUPPORT FITTING AT FAIRING 193AB FWD LEFT SUPPORT FITTING AT FAIRING 193AB WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01.
Part: FITTING — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION AFT RH FLOOR FITTING ON ACCESS 306 (1EA) ON GALLEY 3. AFT RH FLOOR FITTING ON ACCESS 306 (1EA) (PN: CDSP2019-7C-650) ON GALLEY 3 WAS REPLACED PER ZODIAC AEROSPACE CMM 25-33-18
Part: FITTING — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON FITTING (2EA) ON CORNER ACCESS 205 AND UNDER THE FLASHLIGHT AT GALLEY 2 SUMMARY OF NRC 00502: FITTING (2EA) ON CORNER ACCESS 205 AND UNDER THE FLASHLIGHT AT GALLEY 2 WERE REPLACED PER SAFRAN CMM 25-32-84
Part: FITTING — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON FITTING (2EA) ON CORNER ACCESS 205 AND UNDER THE FLASHLIGHT AT GALLEY 2. FITTING (2EA) ON CORNER ACCESS 205 AND UNDER THE FLASHLIGHT AT GALLEY 2 WERE REPLACED PER SAFRAN CMM 25-32-84
Part: ANGLE — CRACKED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CRACK ON REINFORCEMENT ANGLE LOCATED BTW FRAME FS310 AND 25R TO 26R WAS FOUND CRACK ON REINFORCEMENT ANGLE LOCATED BTW FRAME FS310 AND 25R TO 26R WAS REPAIRED PER CRJ900 SRM 53-00-06-201-001-A03
Part: SKIN — CRACKED · airframe 27,630 hrs · 21,175 cycles
SECONDARY NRC FROM NRC 00115: AFTER STIFFENETR REMOVAL, CRACK WAS FOUND ON SKIN OF ACCESS PANEL 171CL. SKIN OF ACCESS PANEL 171CL WAS REPAIRED PER REO 670-53-82-430 REV:--
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON STRINGER SPLICE 25RH IN FS= 327 TO FS= 337 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER SPLICE 25RH IN FS= 327 TO FS= 337 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS AND STRINGER SPLICE WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 , CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 53-00-00-101-001-A01
Part: DRAG ANGLE — CRACKED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CRACKED FWD AND AFT DRAG ANGLE AT RIGHT STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACKED FWD AND AFT DRAG ANGLE AT RIGHT STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WERE REPAIRED PER CRJ-900 SRM 51-42-21-001-001-A01 ,CRJ900 SRM 51-42-06-001-001-A01,CRJ900 SRM 51-42-22-001-001-A01 AND CRJ900 SRM 55-31-00-201-001-A01
Part: SKIN — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
AFTER REMOVAL INTERNAL PRODUCTION DOUBLER, CORROSION ON FUSELAGE INNER SKIN, BETWEEN FS= 295 TO FS= 310 AND STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS FOUND CORROSION ON FUSELAGE INNER SKIN, BETWEEN FS= 295 TO FS= 310 AND STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-01-101-002-A04 AND WAS REPAIRED PER REO 690-53-21-2123 REV --
Part: STRINGER — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON STRINGER 27 IN FS= 349 TO FS= 364 AT MAIN AVIONICS COMPARTMENT DUE TO EXCESSIVE CORROSION ON STRINGER 27 IN FS= 349 TO FS= 364 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ/900 SRM 51-10-06-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: STRINGER — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON STRG 20RH BTW FS364 TO FS379 AT MAIN AVIONICS COMPARTMENT STRG 20RH BTW FS364 TO FS379 AT MAIN AVIONICS COMPARTMENT WAS REPAIRED PER EA CRJ953-20530 REV. IR
Part: STRINGER — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON STRG 24RH BTW FS280 TO FS295 AT MAIN AVIONICS COMPARTMENT. STRG 24RH BTW FS280 TO FS333 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 & CRJ/900 SRM 51-42-21-001-001-A01
Part: ANGLE — CRACKED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CRACK ON PREVIOUS ANGLE REPAIR FS 280 RBL 12 AT E/E COMPARTMENT. ANGLE REPAIR FS 280 RBL 12 AT E/E COMPARTMENT WAS REPAIRED PER REO 690-53-11-1141 REV --
Part: STRINGER — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON STRG 23RH BTW FS349 TO FS364 AT MAIN AVIONICS COMPARTMENT CORROSION ON STRG 23RH BTW FS349 TO FS364 AT MAIN AVIONICS COMPARTMENT WAS EVALAUTED OUT OF LIMITS , THEREFORE WAS REPLACED PER CRJ 900 SRM 53-00-00-101-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON STRG 21RH BTW FS364 TO FS379 AT MAIN AVIONICS COMPARTMENT CORROSION ON STRG 21RH BTW FS364 TO FS379 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS , THEREFORE WAS REPLACED PER CRJ-900 SRM 53-00-00-101-001-A01 AND SRM 51-42-06-001-001-A01 .
Part: STRINGER — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON STRG 25RH BTW FS 295 TO FS 326 AT MAIN AVIONICS COMPARTMENTT. STRG 25RH BTW FS 280 TO FS 326 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: CHANNEL — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON INTERNAL PRODUCTION DOUBLER OF ANTENNA IN FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. PRODUCTION DOUBLER LOCATED ON FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS AND WAS REPLACED PER CRJ900 SRM 53-00-00-101-001-A01,CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-06-001-001-A01 AND TCAS OMNIDIRECTIONAL ANTENNA WAS REPLACED PER CRJ-900 AMM 34-43-07-000-801-A03 AND AMM 34-43-07-400-801-A01
Part: CHANNEL — CORRODED (ZONE 500) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON SEVERAL CHANNEL NUT BTW WS 148.01 TO WS 48.00 LEFT WING FRONT SPART FORWARD, LOWER SECTION. DUE TO EXCESSIVE CORROSION ON SEVERAL CHANNEL NUT BTW WS 148.01 TO WS 48.00 LEFT WING FRONT SPART FORWARD, LOWER SECTION WERE REPLACED PER CRJ900 SRM 51-10-06-001-001-A01 AND SRM 51-42-06-001-001-A01
Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CRACK ON ANGLE FS 280 RBL 25 AT E/E COMPARTMENT. ANGLE ON FS 280 RBL 25 AT E/E COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01 .
Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CRACK ON ANGLE SUPPORTS (2EAS) BTW FS=1000, STGR 8LH AND FS= 1051.30, STGR 7LH ANGLE SUPPORTS (2EAS) BTW FS=1000, STGR 8LH AND FS= 1051.30, STGR 7LH WERE FABRICATED AND REPLACED PER EA CRJ953-21721 REV IR , EA CRJ953-21787 REV IR , CRJ 900 SRM 51-42-06-001-001-A01AND SRM 51-42-21-001-001-A01.
Part: ANGLE — CRACKED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CRACK ON ANGLE SUPPORTS (2EAS) BTW FS=1000, STGR 8LH AND FS= 1051.30, STGR 7LH ANGLE SUPPORTS (2EAS) BTW FS=1000, STGR 8LH AND FS= 1051.30, STGR 7LH WERE FABRICATED AND REPLACED PER EA CRJ953-21721 REV IR , EA CRJ953-21787 REV IR , CRJ 900 SRM 51-42-06-001-001-A01AND SRM 51-42-21-001-001-A01.
Part: CHANNEL — CORRODED (ZONE 600) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON SEVERAL CHANNEL NUT BTW WS 178.00 TO WS 88.00 RIGHT WING FRONT SPART FORWARD, LOWER SECTION. DUE TO EXCESSIVE CORROSION ON SEVERAL CHANNEL NUTS BTW WS 178.00 TO WS 88.00 RIGHT WING FRONT SPART FORWARD, LOWER SECTION WERE REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01 AND CRJ 900 SRM 51-42-06-001-001-A01
Part: BRACKET — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON MACHINED FITTINGS BTW FS519.64 TO FS631.34, & STGR 24RH AND &22 LH (10EAS) AT INTERNAL STRUCTURE OF FWD BAGGAGE BAY. DUE TO EXCESSIVE CORROSION ON MACHINED FITTINGS BTW FS FS519.64 TO FS631.34, & STGR 24RH AND &22 LH (9EAS) AT INTERNAL STRUCTURE OF FWD BAGGAGE BAY WERE REPLACED PER CRJ/900 SRM 53-32-58-101-101-A01 AND SRM 51-42-21-001-001-A01 AND SRM 51-42-13-001-001-A01
Part: RIB — CORRODED (ZONE 500) · airframe 27,630 hrs · 21,175 cycles
CRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT LEFT WING. MACHINED RIB OF LEADING EDGE SS58.41 AT LEFT WING WAS REPAIRED PER REO 690-57-41-240 REV. - -.
Part: STRAP — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB STRAP P/N: CC670-39052-4S AND STRAP P/N: CC670-39052-3S ON FAIRING ACCESS PANEL 193AB WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 AND CRJ-900 SRM 51-42-06-001-001-A01.
Part: STRAP — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION AT SUPPORT STRUCTURE STRAP BTW FAIRING ACCESS PANEL 193AL & 193AR TO FAIRING ACCESS PANEL 193AB STRAP P/N: CC670-39052-4S AND STRAP P/N: CC670-39052-3S ON FAIRING ACCESS PANEL 193AB WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 AND CRJ-900 SRM 51-42-06-001-001-A01.
Part: ANGLE — CRACKED · airframe 27,630 hrs · 21,175 cycles
CRACK ON ATTACHMENT ANGLE OF ACCESS PANEL 542AZ AT MLG SHOCK STRUT BAY ANGLE ON ACCESS PANEL 542AZ AT MLG SHOCK STRUT BAY WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50) WAS REPAIRED PER REO 690-53-11-2156 REV. - - .
Part: RIB — CRACKED (ZONE 500) · airframe 27,630 hrs · 21,175 cycles
CRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT RIGHT WING. CRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT RIGHT WING WAS REPAIRED PER 690-57-41-240 REV - -
Part: RIB — CORRODED (ZONE 500) · airframe 27,630 hrs · 21,175 cycles
CRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT LEFT WING. MACHINED RIB OF LEADING EDGE SS58.41 AT LEFT WING WAS REPAIRED PER REO 690-57-41-240 REV. - -.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON RH SIDE SEAT RAILS, (1 SECTION) FROM FS379 TO FS483 AND (1 SECTION) FROM FS661+16 TO FS661+90 AT PAX CABIN CORROSION ON RH SIDE SEAT RAILS, (1 SECTION) FROM FS379 TO FS483 AND (1 SECTION) FROM FS661+16 TO FS661+90 AT PAX CABIN WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 EVALUATED OUT LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02, SRM 53-21-49-101-001-A01 THEREFORE WERE REPLACED PER CRJ-900 AMM 53-00-49-000-801 (CONFIG A12) AND AMM 53-00-49-400-801 (CONFIG A12)
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON RT SIDE SEAT RAILS, (1 SECTION) FROM FS744 TO FS761, (1 SECTION) FROM FS785 TO FS847 AND (1 SECTION) FROM FS847+16 TO FS897 AT PAX CABIN. DUE TO EXCESSIVE DAMAGE ON RH SIDE SEAT RAILS, THE SECTIONS FROM FS 785 TO FS 847 AND FROM FS 847+16 TO FS 897 IN THE PAX CABIN WERE REPLACED PER CRJ-900 SRM 53-41-49-101-001-A02, SRM 53-51-49-101-001-A02, AND AMM 53-00-49
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON RH SEAT RAILS RBL9, (1 SECTION) FROM FS581 TO FS661+32, (1 SECTION) FROM FS661+32 TO FS677 AND (1 SECTION) FROM FS677 TO FS847+16 AT PAX CABIN. CORROSION ON RH SEAT RAILS RBL9, (1 SECTION) FROM FS581 TO FS661+32, (1 SECTION) FROM FS661+32 TO FS677 AND (1 SECTION) FROM FS677 TO FS847+16 AT PAX CABIN WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED OUT OFF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02, SRM 53-31-49-101-001-A02 AND WERE REPLACED PER CRJ 900 AMM 53-00-49
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON LH SEAT RAILS LBL9, (1 SECTION) FROM FS847+16 TO FS988 AND (1 SECTION) FROM FS988 TO FS1000 AT PAX CABIN. CORROSION ON LH SEAT RAILS LBL9, (1 SECTION) FROM FS847+16 TO FS988 AND (1 SECTION) FROM FS988 TO FS1000 AT PAX CABIN WAS REMOVED CRJ900 SRM 51-21-06-001-001-A01 AND EVALUATED OUT OFF LIMITS PER CR-J900 SRM 53-51-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON LH SIDE SEAT RAILS, (2 SECTIONS) FROM FS379 TO FS 573 AND (4 SECTIONS) FROM FS573 TO FS669 AT PAX CABIN. CORROSION ON LH SIDE SEAT RAILS, (2 SECTIONS) FROM FS379 TO FS 573 AND (4 SECTIONS) FROM FS573 TO FS669 AT PAX CABIN WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 EVALUATED OUT LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02, SRM 53-21-49-101-001-A01 THEREFORE WERE REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01, AMM 53-00-49-000-801 (CONFIG A12) AND AMM 53-00-49-400-801 (CONFIG. A12)
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON RH SEAT RAIL RBL9 (1 SECTION) 847+16 TO FS977 AT PAX CABIN. CORROSION ON RH SEAT RAIL RBL9 (1 SECTION) 847+16 TO FS977 AT PAX CABIN WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 EVALUATED OUT LIMITS PER CRJ-900 SRM 53-51-49-101-001-A02 THEREFORE WAS REPLACED PER CRJ 900 AMM 53-00-49-000-801 (CONFI A12) AND PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A12)
Part: SUPPORT PLATE — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON RH/LH MLG HYDRAULIC LINES SUPPORTS PLATE (4EA) (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA. RH/LH MLG HYDRAULIC LINES SUPPORTS PLATE (4EA) (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA WERE EVALUATED OUT OF LIMITS AND WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 ,CRJ900 SRM 51-41-02-001-001-A01 AND CRJ900 SRM 53-00-00-101-001-A01
Part: SUPPORT PLATE — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON RH/LH MLG HYDRAULIC LINES SUPPORTS PLATE (4EA) (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA. RH/LH MLG HYDRAULIC LINES SUPPORTS PLATE (4EA) (IN BK, LG EXT, LG RET) ON WHEEL WELL AREA WERE EVALUATED OUT OF LIMITS AND WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 ,CRJ900 SRM 51-41-02-001-001-A01 AND CRJ900 SRM 53-00-00-101-001-A01
Part: POST — CORRODED (OZN E200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON FLOOR POST, LOWER SECTION LOCATED BTW FS 280 AND STGR 25LH. FLOOR POST, LOWER SECTION LOCATED BTW FS 280 AND STGR 25LH WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-13-001-001-A01 SRM 51-42-10-001-001-A01
Part: POST — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON FLOOR POST, LOWER SECTION LOCATED BTW FS 280 AND STGR 25RH. FLOOR POST, LOWER SECTION LOCATED BTW FS 280 AND STGR 25RH WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON LH SEAT RAILS LBL26 (1 SECTION) FROM FS 927 TO FS977 AT PAX CABIN CORROSION ON LH SEAT RAIL LBL26 (1 SECTION) FROM FS 927 TO FS977 AT PAX CABIN WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-A01 AND SRM 53-51-49-101-001-A02 THEREFORE WAS REPLACED PER CRJ-900 AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.
Part: FRAME — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON FRAME FS349 BTW STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. CORROSION ON FRAME FS349 BTW STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS AND FRAME FS349 WAS REPLACED PER CRJ900 SRM 51-10-06-001-001-A01,CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON LH SIDE SEAT RAIL, (3 SECTIONS) FROM FS785 TO FS900 AND (1 SECTION) FROM FS915 TO FS977 CORROSION ON LH SIDE SEAT RAIL, (3 SECTIONS) FROM FS785 TO FS900 AND (1 SECTION) FROM FS915 TO FS977 WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND WERE REPLACED CRJ-900 AMM 53-00-49
Part: WEB — CRACKED (ZONE 200) · airframe 27,630 hrs · 21,175 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 CRJ900 SRM 53-11-43-201-001-A01
Part: STAND OFF — CRACKED (ZONE 400) · airframe 27,630 hrs · 21,175 cycles
CRACKED INNER SUPPORT ANGLE (STANDOFF 1 EA) ON RH UPPER TRANSCOWL. INNER SUPPORT ANGLE (STANDOFF 1 EA) ON RH UPPER TRANSCOWL WAS REPLACED PER CRJ-900 SRM 51-42-28-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: STIFFENER — CRACKED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CRACK ON STIFFENER (1EA) ON ACCESS PANEL 171CL STIFFENER ON ACCESS PANEL 171CL WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
Part: WEB — CRACKED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CRACKED FLOOR WEB RIGHT SIDE AT_ ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS193.00. FLOOR WEB RIGHT SIDE AT_ ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.
Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CRACK ON CORNERS OF (BRACKET ASSY) MAIN BATTERY DIRECT BUS (JB6) AT FWD EQPT COMPT (BRACKET ASSY) MAIN BATTERY DIRECT BUS (JB6) AT FWD EQPT COMPT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01.
Part: BRACKET — CORRODED (ZONE 800) · airframe 27,630 hrs · 21,175 cycles
CRACK ON UPPER STABILIZER BRACKET AT GALLEY SERVICE DOOR UPPER STABILIZER BRACKET AT GALLEY SERVICE DOOR WAS REPLACED PER CRJ 900 AMM 52-41-27
Part: DIAPHRAGM — CRACKED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CRACK ON DIAPHRAGM AT FWD AREA OF MLG W/W BTW FS= 797 TO FS= 807 LBL/RBL 35. (2EA). DIAPHRAGM (2EA) AT FWD AREA OF MLG W/W BTW FS= 797 TO FS= 807 LBL/RBL 35 WERE REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 & SRM 51-41-02-001-001-A01
Part: HINGE — CRACKED (ZONE 800) · airframe 27,630 hrs · 21,175 cycles
CRACK ON HINGES (2EAS) IN STEP PANEL 832ET, 832FT (1EA), AT PASSENGER DOOR. (L1) (PTAS) HINGE (2EAS) IN STEP PANEL 832ET WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-41-02-001-001-A01 AND CRJ-900 AMM 20-21-00-910-801 (CONFIG A01), HINGE (1EA) IN STEP PANEL 832FT WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01.
Part: HINGE — CRACKED (ZONE 800) · airframe 27,630 hrs · 21,175 cycles
CRACK ON HINGES (2EAS) IN STEP PANEL 832ET, 832FT (1EA), AT PASSENGER DOOR. (L1) (PTAS) HINGE (2EAS) IN STEP PANEL 832ET WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-41-02-001-001-A01 AND CRJ-900 AMM 20-21-00-910-801 (CONFIG A01), HINGE (1EA) IN STEP PANEL 832FT WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01.
Part: BRACKET — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON BOTH SUPPORT (2EA) OF ELECTRICAL CONECTORS PX19, PX34, PX17 AND PX33 AT MLG WHEEL WELL SUPPORT (2EA) OF ELECTRICAL CONECTORS PX19, PX34, PX17 AND PX33 AT MLG WHEEL WELL WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
Part: PROTECTOR — CRACKED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CRACK ON HARNESS PROTECTOR OF FWD HINGE ARM AT CENTER BAGGAGE BAY DOOR HARNESS PROTECTOR OF FWD HINGE ARM AT CENTER BAGGAGE BAY DOOR WAS REPAIRED PER EA CRJ952-21859 REV. IR
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON MID CAP ANGLE OF LOWER SILL AREA AT PASSENGER DOOR CUTOUT MID CAP ANGLE OF LOWER SILL AREA AT PASSENGER DOOR CUTOUT WAS REPLACED BY EXCESSIVE CORROSION PER CRJ900 SRM 53-21-23-101-001-A02 AND SRM 51-41-02-001-001-A01
Part: SUPPORT — CORRODED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON BOTH SUPPORT (2EA) OF ELECTRICAL CONECTORS PX19, PX34, PX17 AND PX33 AT MLG WHEEL WELL SUPPORT (2EA) OF ELECTRICAL CONECTORS PX19, PX34, PX17 AND PX33 AT MLG WHEEL WELL WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01
Part: STRIKER — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON STRIKER SEAL OF LOWER SILL AREA AT SERVICE DOOR CUTOUT STRIKER SEAL OF LOWER SILL AREA AT SERVICE DOOR CUTOUT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01.
Part: DIAPHRAGM — CRACKED (ZONE 100) · airframe 27,630 hrs · 21,175 cycles
CRACK ON DIAPHRAGM AT FWD AREA OF MLG W/W BTW FS= 797 TO FS= 807 LBL/RBL 35. (2EA). DIAPHRAGM (2EA) AT FWD AREA OF MLG W/W BTW FS= 797 TO FS= 807 LBL/RBL 35 WERE REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 & SRM 51-41-02-001-001-A01
Part: HINGE — CRACKED (ZONE 800) · airframe 27,630 hrs · 21,175 cycles
CRACK ON HINGES (2EAS) IN STEP PANEL 832ET, 832FT (1EA), AT PASSENGER DOOR. (L1) (PTAS) HINGE (2EAS) IN STEP PANEL 832ET WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-41-02-001-001-A01 AND CRJ-900 AMM 20-21-00-910-801 (CONFIG A01), HINGE (1EA) IN STEP PANEL 832FT WAS REPLACED PER CRJ-900 SRM 51-41-02-001-001-A01.
Part: ANGLE — CORRODED (ZONE 200) · airframe 27,630 hrs · 21,175 cycles
CORROSION ON MOUNTING ANGLE OF LOWER SILL AREA AT SERVICE DOOR CUTOUT DUE TO EXCESSIVE CORROSION ON MOUNTING ANGLE OF LOWER SILL AREA AT SERVICE DOOR CUTOUT WAS REPLACED PER CRJ900 SRM 53-21-23-101-001-A02,CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 , CRJ900 SRM 51-41-02-001-001-A01 AND CRJ900 AMM 53-21-27 (CONFIG A02)
Part: ACCESS PANEL — CORRODED · airframe 27,630 hrs · 21,175 cycles
CORROSION ON ACCESS PANELS 542AZ, 542BZ, 642BZ AND 642AZ (BOTH SIDES) CORROSION ON ACCESS PANELS 542AZ, 542BZ, 642BZ WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WERE EVALUATED WITHIN LIMITS PER CRJ-900 SRM 57-22-32-101-001-A01, AND PANEL 642AZ WAS REPLACED PER CRJ-900 IPC 57-52-32-40
Earlier reports · 2015–2023 · 50 reports
2023
Part: SKIN — CHAFED (BS 942 S27) · airframe 20,865 hrs · 15,523 cycles
SKIN CHAFE AT F.S.942.00 STRINGER 27 REPAIRED FUSELAGE SKIN AT F.S.942 IAW MHI RJ REO 690-53-51-372 REV -- DATED 2023-01-23
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 20,865 hrs · 15,523 cycles
FWD VERTICAL STABILIZER DRAG ANGLE IS CRACKED NEAR 67.5% REAR SPAR DATUM (LH) REPAIRED LH FWD VERTICAL STABILIZER DRAG ANGLE IAW CRJ 900 SRM 55-31-00-201-001-A01
Part: FORMER — CRACKED (EMERGENCY EXIT) · airframe 20,865 hrs · 15,523 cycles
L/H FWD OVER WING EMERGENCY EXIT DOOR S/N SB1366 UPPER FORMER IS CRACKED. REPAIRED L/H FWD OVERWING EMERGENCY EXIT DOOR S/N SB1366 IAW MHIRJ REO 690-52-21-132 REV A DATED 2023-01-23
Part: FLOORBEAM — CORRODED (BS 280 L-RBL12) · airframe 20,865 hrs · 15,523 cycles
BS 280 FWD J ANGLE WAS CORRODED. REMOVED THE FORWARD ANGLE BETWEEN LBL 12 AND RBL 12 IAW SRM 51-42-21-001-001-A01. INSTALLED A NEW SERVICABLE ANGLE IAW SRM 51-40-11-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: ANGLE — CORRODED (DOOR SILL) · airframe 20,865 hrs · 15,523 cycles
"PAX DOOR UPPER SILL ANGLE IS CORRODED. REPLACED CAP ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 "
Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 20,865 hrs · 15,523 cycles
PAX DOOR LOWER SILL ANGLE IS CORRODED. REMOVED UNSERVICEABLE PAX DOOR LOWER SILL ANGLE P/N SH670-31875-7 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01. CORRECTIVE ACTION: INSTALLED PAX DOOR SILL ANGLE IAW CRJ-900 SRM 51-42-06-001-001-AO1
Part: PLATE — CORRODED (FWD CARGO DOOR) · airframe 20,865 hrs · 15,523 cycles
FWD BAGGAGE BAY DOOR LOWER PLATE IS DAMAGED. REPLACED FWD BAGGAGE BAY DOOR LOWER PLATE IAW CRJ 900 SRM 51-41-02-001-001-A01. INSTALLED DOME-NUT ON LOWER PLATE IAW CRJ900 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW BAGGAGE BAY DOOR PLATE IAW CRJ 900 51-40-11-001-001-A01.
Part: FLOORBEAM — CORRODED (BS 280 LBL 12) · airframe 20,865 hrs · 15,523 cycles
L/H FS LOWER WEB IS CORRODED AT LBL 12 BETWEEN CORROSION CAP AND WEB. REPAIRED FS 280 LH WEB IAW CRJ 900 SRM 53-11-10-201-004-A01.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,865 hrs · 15,523 cycles
L/H FS 280 BEAM IS CORRODED REPLACED LH FS280 CROSSBEAM (P/N: CC670-34094-1) IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 20,865 hrs · 15,523 cycles
R/H FS 280 BEAM IS CORRODED REPLACED RH FS280 CROSSBEAM (P/N: CC670-34094JP-2S) IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
Part: WEB — CORRODED · airframe 20,865 hrs · 15,523 cycles
R/H WEB IS CORRODED AT RBL 36 REPAIRED RH WEB IAW CRJ 900 SRM 53-11-10-201-004-A01.
Part: SEAT TRACK — CORRODED (BS 349-364 RBL9) · airframe 20,865 hrs · 15,523 cycles
SEAT TRACK @ RBL9 FROM FS349 TO FS364 IS CORRODED REMOVED CORRODED SEAT TRACK AND INSTALLED NEW SERVICEABLE SEAT TRACK AT RBL9 BETWEEN FS 349 AND 477 IAW CRJ 900 AMM 53-00-49-000-801-A12.
Part: DOOR SILL — CORRODED (BS 1000-1031) · airframe 20,865 hrs · 15,523 cycles
"AF CARGO DOOR SILL IS CORRODED BETWEEN F.S. 1000.0 TO F.S. 1031.00. REMOVED AND REPLACED AFT CARGO DOOR SILL PLATE PN MM670-35655-003 IAW CRJ 900 SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-21-001-001-A01 "
2019
Part: ANGLE — CORRODED · airframe 13,537 hrs · 9,356 cycles
"INITIAL INSPECTION. CORROSION ON ANGLES (4EAS) AT SERVICE DOOR SORROUND STRUCTURE LOWER SILL (ON FITTINGS OF PROTECTOR PLATE). (SM)(CPAX)(TCI53-20-320) "ANGLES (4EAS) AT SERVICE DOOR SORROUND STRUCTURE LOWER SILL WERE REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A01.
Part: CANISTER — CRACKED (SLAT TRACK) · airframe 13,537 hrs · 9,356 cycles
CRACK ON SLAT TRACK CANISTER 1-3 AT RH WING MAIN FUEL TANK WS 148. (SM)(AD). CRACK ON SLAT TRACK CANISTER 1-3 AT RH WING MAIN FUEL TANK WS 148 WAS REPAIRED PER REO 670-57-42-577 REV.
Part: ANGLE — CORRODED (DOOR SILL) · airframe 13,537 hrs · 9,356 cycles
CORROSION ON MID CAP ANGLE AT PASSENGER DOOR SURROUND STRUCTURE LOWER SILL.(SM)(CPAX)(53-20-319). "MID CAP ANGLE AT PASSENGER DOOR SURROUND STRUCTURE LOWER SILL WAS REPLACED FOR A NEW ONE (P/N: SH670-31825-9) PER CRJ-900 SRM 51-41-02-001-001-A01.
Part: STRIKER — CORRODED (SERVICE DOOR) · airframe 13,537 hrs · 9,356 cycles
INITIAL INSPECTION. CORROSION ON STRIKER SEAL AT SERVICE DOOR SORROUND STRUCTURE LOWER SILL (SM)(CPAX)(TCI 53-20-320) SUMMARY: STRIKER SEAL AT SERVICE DOOR SORROUND STRUCTURE LOWER SILL WAS REPLACED PER CRJ-900 S.R.M. 51-42-06-001-001-A01.
Part: DOOR SILL — CORRODED (BS 319-349) · airframe 13,537 hrs · 9,356 cycles
INITIAL INSPECTION: CORROSION ON LOWER SILL AT GALLEY SERVICE DOOR FS=319.70 TO FS=349 (CPAX) SUMMARY OF NRC S/N 00176: LOWER SILL WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: INTERCOSTAL — CORRODED (349-364) · airframe 13,537 hrs · 9,356 cycles
CORROSION ON INTERCOSTAL 2 LBL, 2 RBL BTW FS 364-349. AT E/E COMPARTMENT. (EE) (SM) INTERCOSTALS 2 LBL AND 2 RBL BTW FS 364-349 WERE REPLACED PER CRJ 900SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 (LEVEL CORROSION 2)
Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,537 hrs · 9,356 cycles
INITIAL INSPECTION: CRACKED LONGITUDINAL FLOOR BEAM RBL 12 AND FS 280. BELOW COCKPIT. CRACKED LONGITUDINAL FLOOR BEAM RBL 12 AND FS 280. BELOW COCKPIT WAS REPAIRED PER REO: 690-53-11-1141.REV.
Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 13,537 hrs · 9,356 cycles
CORROSION ON FLOOR SEAT RAILS 9RBL FS364 TO FS485, 9LBL FS374 TO FS485, 27LBL FS350 TO FS485 AT PAX CABIN. (CPAX)(TCI 53-20-318) SUMMARY OF NRC S/N 00112: FLOOR SEAT RAILS 9RBL FS364 TO FS485, 9LBL FS374 TO FS485, 27LBL FS350 TO FS485 AT PAX CABIN WERE REPLACED PER CRJ-900 AMM 53-00-49-400-801 (CONFIG A12) (LEVEL CORROSION 2).
Part: SEAT TRACK — CORRODED (BS 672-986) · airframe 13,537 hrs · 9,356 cycles
CORROSION ON SIDE SEAT RAILS STGR 15 LH/RH AT FS672 TO FS722, FS743 TO FS763, FS785 TO FS847+14, FS847+14 TO FS907, FS907 TO FS986. PAX CABIN. AT PAX CABIN. (CPAX)(TCI 53-20-318) SUMMARY OF NRC S/N 00111: SEAT RAILS STGR 15 LH/RH 677 TO FS722, FS743 TO FS763, WERE REPLACED PER CRJ-900 AMM TASK 53-00-49-400-801 (CONFIG A12). SEAT RAILS STGR 15 LH/RH AT FS672 TO 677, FS785 TO FS847+14, FS847+14TO FS907, FS907 TO FS986. WERE CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND WAS RE-INSPECTED AND NO CORROSION WAS FOUND PER CRJ 900 SRM 51-11-00-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 517-723) · airframe 13,537 hrs · 9,356 cycles
CORROSION ON FLOOR SEAT RAILS IN SECTIONS FS=661+62.0 TO FS=661+46.0 (9LBL/9RBL)/ FS= 661 TO FS=645 (9LBL/9RBL)/ FS=597 (9LBL/9RBL/ FS= 533 TO FS= 517 (9RBL) (PAX CABIN) TCI: 53-20-245 SEAT RAILS IN SECTIONS FS661+62.0 TO FS661+46.0 (9LBL/9RBL) / FS661 TO FS645 (9LBL/9RBL) / FS597 (9LBL/9RBL / FS533 TO FS517 (9RBL) WERE REPLACE PER CRJ-900 AMM TASK 53-00-49-400-801 (CONFIG A12) (LEVEL CORROSION 2).
Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,537 hrs · 9,356 cycles
INITIAL INSPECTION: CRACKED LONGITUDINAL FLOOR BEAM LBL 12 AND FS 280. BELOW COCKPIT. CRACKED LONGITUDINAL FLOOR BEAM LBL 12 AND FS 280. BELOW COCKPIT WAS REPAIRED PER REO: 690-53-11-1141.REV.
Part: FRAME — CORRODED (BS 295) · airframe 13,537 hrs · 9,356 cycles
CORROSION ON FRAME IN STA. FS:295 BETWEEN STGR:26RH-26LH.(EE) (SM) CORROSION ON FRAME IN STA. FS:295 BETWEEN STGR:26RH-26LH WAS REPAIRED PER EA NO: CRJ953-09006 REV IR. (LEVEL CORROSION 2)
Part: FRAME — CORRODED (BS 310) · airframe 13,537 hrs · 9,356 cycles
INITIAL INSPECTION: CORROSION ON FRAME IN STA. FS:310 BETWEEN STGR:25RH-26LH. (EE) (SM). CORROSION ON FRAME IN STA. FS:310 BETWEEN STGR:25RH-26LH WAS REPAIRED PER EA NO: CRJ953-09050 REV IR. (LEVEL CORROSION 2)
Part: SEAT TRACK — CORRODED (BS 485-898) · airframe 13,537 hrs · 9,356 cycles
INITIAL INSPECTION: CORROSION ON FLOOR SEAT RAILS 27 LBL FS485 TO FS581, FS581 TO FS661+32, FS661+32 TO FS692.97. 9 LBL/RBL FS485 TO FS581, FS581 TO FS661+32, FS661+32 TO FS683.5, FS691 TO FS836.5, FS836.5 TO FS847+51. AT PAX CABIN. (CPAX)(TCI 53-20-318) SEAT RAILS 27 LBL FS485 TO FS581,AND SEAT RAILS 9 LBL/RBL FS485 TO FS581, FS581 TO FS661+32, FS661+32 TO FS683.5, FS691 TO FS836.5, FS836.5 TO FS847+51, WERE REPLACED PER CRJ-900 AMM TASK 53-00-49-400-801 (CONFIG A12) LEVEL CORROSION 2. AND SEAT RAILS 27 LBL FS581 TOFS661+32, FS661+32 TO FS692.97. WERE CLEANED PER CRJ-900 SRM 51-26-00-001-001-A01 AND .AND RE-INSPECTED, NO CORROSION WAS FOUND PER CRJ 900 SRM 51-11-00-001-001-A01
Part: SKIN — DAMAGED (BS 253-261) · airframe 13,537 hrs · 9,356 cycles
INITIAL INSPECTION: LIGHTNING STRIKES (3EA) ON EXTERNAL FUSELAGE SKIN, FS253.5, FS259.5 AND FS261 OVER STGR 27. (FUS) LIGHTNING STRIKES (3EA) ON EXTERNAL FUSELAGE SKIN, FS253.5, FS259.5 AND FS261 OVER STGR 27 WERE REPAIRED PER CRJ 900 SRM 53-00-00-201-003-A03.
2018
Part: PUMP — LOW PRESSURE (HYD SYSTEM) · airframe 11,609 hrs · 7,972 cycles
HYD PUMP 3 WENT TO ZERO QUANTITY . CHECKED THE NR 3 HYDRAULIC SYSTEM WITH APU/EXT IAW AMM 29-10-00, OPS CHECKED GOOD. REPLACED THE NR 2 IDG CONTROL UNIT DUE TO B1- 006887, OPS CHECKED GOOD. EMERGENCY DECLARED BY CREW.
Part: SENSOR — MALFUNCTIONED (RT ENG OIL TEMP) · airframe 11,160 hrs · 7,636 cycles
DURING CLIMBOUT, PASSING 10000 FT, RIGHT ENGINE OIL TEMP INDICATED YELLOW WITH NO OIL PRESSURE ABNORMAL INDICATION. OIL TEMP CLIMBED FROM 150 AND THEN WENT RED AT OR ABOVE 165 C. QRH WAS PERFORMED WITH REDUCTION OF THRUST TO GND IDLE. ENGINE OIL TEMP REMAINED YELLOW UNTIL BELOW 11,000 FT. MAX ALTITUDE WAS 18000 FT. ON APPROACH WITH POWER, THERE WAS ALL GREEN, THE RIGHT ENGINE WAS HIGHER THAN THE LEFT ENGINE OIL. MX-MDC RT ENGINE TREND-12:19Z 158 C AT 57 PSI (LT 101C), 12:10Z 74 C AT 74 PSI, NO FAULT, NO HISTORY, REMOVED AND REPLACED THE RIGHT ENGINE TEMP SENSOR IAW AMM 79-31-01. OPS CHECKED GOOD. RIGHT OIL TEMP 112 LEFT OIL TEMP 107.
2017
Part: MEGAPHONE — INOPERATIVE (MAIN CABIN) · airframe 10,211 hrs · 6,932 cycles
MEGAPHONE INOPERATIVE. R & R THE MEGAPHONE IAW AMM 25-61-14. OPS CHECKED GOOD.
Part: OXYGEN MASK — DEPLOYED (FWD LAVATORY) · airframe 10,038 hrs · 6,803 cycles
FORWARD LAV O2 MASKS DEPLOYED NEED RESECURED RESTOWED LAV O2 MASK IAW AMM 35-21-17. OK FOR SERVICE.
Part: ACTUATOR — FAILED (APU) · airframe 9,854 hrs · 6,681 cycles
APU FIRE MASTER WARNING MESSAGE RECIEVED ON GROUND. APU AUTO SHUTDOWN. BOTTLES DID NOT DISCHARGE. TURNED OFF MASTER BATTERY. PERFORMED DOOR RIGGING PROCEDURE IAW AMM 49-14-19. DOOR WILL NOT CLOSE AFTER OPENING. REMOVED AND REPLACED THE APU INLET DOOR ACTUATOR IAW AMM 49-14-16. OPS CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE.
Part: OXYGEN MASK — INOPERATIVE (AFT LAVATORY) · airframe 9,678 hrs · 6,542 cycles
AFT LAVATORY OXYGEN MASK IS INOPERATIVE. REPACKED AFT LAVATORY PAX OXYGEN MASK. ALL CHECKED GOOD IAW AMM 35-21-17.
Part: STOWAGE BOX — LEAKING (OXYGEN MASK) · airframe 9,669 hrs · 6,535 cycles
FIRST OFFICER`S OXYGEN MASK LEAKING. REMOVED & REPLACED THE O2 MASK STOWAGE BOX IAW AMM T.A 35-11-15.
Part: ACM — SEIZED (AC BAY) · airframe 9,567 hrs · 6,460 cycles
CABIN WAS FILLED WITH SMOKE PRIOR TO PUSHBACK WHILE SITTING AT GATE WITH APU RUNNING AND BOTH PACKS SELECTED ON. HAD A L PACK AUTOFAIL CAUTION MSG ALONG WITH L PACK FAULT. OBSERVED DUCT TEM FOR L PACK ABOVE 99 DEGREES C. L PACK FAULT STATUS MSG DUE TO MT023-B1-007373 CAUSED BY PACK OVERTEMP. SHUT DOWN LEFT PACK. VISUALLY INSPECTED L&R PACKS WITH NO VISUAL DAMAGE NOTED. WITH L PACK OFF SMELL WENT AWAY AND TEMP INSIDE COCKPIT REDUCED. LEFT PACK WAS FOUND TO BE LOCKED UP INTERNALLY. REMOVED AND REPLACED ACM IAW AMM 21-51-00 P/N OFF/ON GG670-95009-7 S/N OFF 01799 S/N ON 01317. OPS AND LEAKS CHECKS GOOD.
2016
Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 7,727 hrs · 5,196 cycles
CAPTAIN`S OXYGEN MASK IS LEAKING AIR WHEN THE MASK CONTAINER DOOR COVER IS OPEN AROUND THE FLOW INDICATOR. REMOVED AND REPLACED THE OXYGEN MASK STOWAGE BOX IAW 35-11-15. OPS CHECK COMPLIED AND PASS IAW 23-51-06. LEAK TEST OF THE CREW OXY SYSTEM IAW 35-10-06.
Part: STRAP — BROKEN (FLASHLIGHT ASSY) · airframe 7,237 hrs · 4,846 cycles
FORWARD STRAP ON FLASHLIGHT IS BROKEN. REPLACED THE STRAP AS REQUIRED IAWAMM 25-61-00
Part: LIGHT — UNSECURE (CABIN) · airframe 6,318 hrs · 4,210 cycles
JUMP SEAT DOES NOT BOUNCE BACK UP, FLOOR LIGHTING STRIP CAME LOOSE RT SIDE NEXT TO CARTS. INSTALLED EMERGENCY LIGHT STRIP IAW AMM 33-51-01. OK FOR SERVICE.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 5,891 hrs · 3,920 cycles
RIGHT EXTERIOR EMER LIGHT INOPERATIVE. DEFERRED RT EXTERIOR EMER LIGHT IAW MEL 33-51-2A CAT C PLACARD INSTALLED MMO2 UPDATED MOC NOTIFIED 96211. REPLACED RT AFT EXTERIOR EMER LIGHT ASSEMBLY, PN 2LA004305-75, SN OFF 2215934 & SN ON 1066480 IAW AMM 33-51-15. OPERATIONAL TESTED GOOD, REMOVED MM02, MXC NOTIFIED 95909.
Part: RETAINER — DAMAGED (CARGO DOOR) · airframe 5,707 hrs · 3,796 cycles
FORWARD & CTR BAGGAGE BAY DOORS EACH HAVE DAMAGED SEAL RETAINER AT LOWER INBD, FWD & AFT CORNERS. REPAIRED FWD & CTR CARGO BAY DOOR SEAL RETAINERS. REF STEPS 1 - 2 FOR WORK PERFORMED.
Part: WEB — CRACKED (PAX DOOR) · airframe 5,707 hrs · 3,796 cycles
PASSENGER DOOR HAS MULTIPLE CRACKS IN FWD & AFT WEBS. CONTINUATION CARD 81529711 OP 71. REPAIRED PAX DOOR AFT WEB IAW EO 670-52-11-104 REV F IAW STEPS 1 - 8 FOR WORK PERFORMED.
Part: HOUSING — CRACKED (E&E DOOR) · airframe 5,707 hrs · 3,796 cycles
MAIN AVI DOOR HANDLE HOUSING HAS 2 EACH CRACK INDICATIONS NOTED AROUND BASE OF SHAFT AT AFT SIDE, 90% FSH. FAILED NDT INSPECTION. CONTINUATION CARD 81529711 OP 74 INSTALLED NEW AVI DOOR HANDLE HOUSING PN 601R31053-3 & SN 1156. REF JOB 8152971 OP 48 STEPS 1 - 6 FOR WORK PERFORMED.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 5,707 hrs · 3,796 cycles
AFT BELLY FAIRING PANEL 195DL, SPLICE ANGLE IS CRACKED. REMOVED CRACKED ANGLE, RECEIVED NEW ANGLE PN CC690-39251-1. PERFORMED EO R53573 REVISION 1, REVISION DATE 29 JAN 16.
2015
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 4,848 hrs · 3,256 cycles
FLIGHT ATTENDANT ALT JS FLASHLIGHT IS INOPERATIVE. DEFERRED JS ALT FLASHLIGHT IAW MEL 25-61-4A. ENTERED INMM02 & PLACARD INSTALLED.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 4,735 hrs · 3,162 cycles
FOUND GALLEY FLASHLIGHT INOPERATIVE, RT SIDE OF GALLEY. DEFERRED GALLEY FLASHLIGHT RT SIDE IAW MEL 25-61-4A C. MXC NOTIFIED 96045.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 4,134 hrs · 2,744 cycles
FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R FWD NR 2 FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW CMM 25-60-02. OPERATIONS CHECKED GOOD AT THIS TIME.
Part: DOOR SEAL — LEAKING (ESCAPE HATCH) · airframe 3,925 hrs · 2,597 cycles
EMERGENCY ESCAPE HATCH ON THE FRONT CORNER CLOSER TO CAPTAINS SIDE LEAKS. ALSO, A LEAK ONTO CAPTAINS SIDE CHART CLIP. REMOVED CREW ESCAPE HATCH, INSPECTED OUTER HANDLE SEAL & DOOR TO FUSELAGE SEAL IAW AMM 55-22-07. CLEANED & REAPPLIED LUBRICATION IAW AMM 12-20-52. FOUND SEALS INTACT WITHOUT ANY DEFECTS. INSTALLED CREW ESCAPE HATCH IAW AMM 55-22-07.AIRCRAFT OK FOR SERVICE.
Part: TRIM PANEL — DEFECTIVE (ESCAPE HATCH) · airframe 3,252 hrs · 2,143 cycles
CREW REPORTED WATER LEAK FROM COCKPIT ESCAPE HATCH & ALSO WATER DRIPS FROM OVERHEAD INSTRUMENT PANELS. R & R CREW HATCH OUTER TRIM PANEL IAW 25-16-06. NOTED DAMAGE RT AFT CORNER OF TRIM PANEL, PROBLEM RECTIFIED.
Part: UNKNOWN — LEAKING (ESCAPE HATCH) · airframe 3,200 hrs · 2,110 cycles
CREW ESCAPE HATCH LEAKING WATER. INSPECTED CREW ESCAPE HATCH AS REQUIRED. DOOR SEAL CONDITION GOOD. ACFT GOOD FOR SERVICE.