N690CA
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.
152 reports on file, 2005-11-14 – 2025-05-09.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 34,783 hrs · 26,207 cycles
FLOOR SUPPORT AT PAX DOOR FS310-FS333 HAS CORROSION. REMOVED AND INSTALLED NEW SERVICEABLE PAX DOOR MID CAP ANGLE PN# SH670-31825-9S IAW CRJ 51-41-02-001-001-A01 AND 51-41-04-001-001-A01.
Part: SKIN — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
F.S. 533-581 BAGGAGE DOOR SURROUND CORRODED, FWD AND CENTER TOP PLATES CORRODED IN MULTIPLE PLACES. REPAIRED FORWARD BAGGAGE BAY INNER CLOSING SKIN IAW ENDEAVOR AIR EA CRJ753-18690 REV IR DATED 3/17/2025
Part: HINGE — DAMAGED (ZONE 200) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR HINGE AFT ROLL PIN HOLE IS ELONGATED COMPLIED WITH MHIRJ REO# 670-52-11-1467 REV. -- DATED 3-13-2025 IN REPAIR OF DAMAGED SPRING PIN HOLE PAX DOOR HINGE
Part: HINGE — WORN (ZONE 200) · airframe 34,783 hrs · 26,207 cycles
AFT MOST OUTER LUGS (10 EA.) ON PAX DOOR HINGE (FUSELAGE SIDE) HAVE INNER DIAMETERS THAT ARE WORN BEYOND THE ALLOWABLE LIMITS OF CRJ 700 SRM 53-21-23-201-010-A01, STEP 1A. REMOVED LOWER STRIKER P/N SH670-31886-1 AND DRAIN TUBE P/N SH670-31904-3 IAW CRJ700 SRM 51-42-21-001-001-A01. REMOVED WORN FUSELAGE SIDE PAX DOOR HINGE AND INSTALLED NEW SERVICEABLE HINGE IAW CRJ700 SRM 53-21-23-201-007-A01. P/N SH670-31876-13S INSTALLED LOWER STRIKER P/N SH670-31886-1 AND DRAIN TUBE P/N SH670-31904-3 IAW CRJ700 SRM 51-42-21-001-001-A01.
Part: ANGLE — NOT REPORTED · airframe 34,783 hrs · 26,207 cycles
FABRICATION REQUIRED OF REINFORCEMENT JOINT ANGLE STA 310 & 349 PN SH670-31947-4. PART REQUIRED FOR MWC BARCODE HN00221783 S/N: 00795. LOCATED AND DRILLED REINFORCEMENT JOINT ANGLE STA 310 & 349 FOR EXAMPLE OF P/N SH670-31947-4 FROM 7075-0 0.040ÿ½ PO# 5-59801 REFERENCING DRW SH670-31947 REV. NC AND AS PER SAMPLE IAW CRJ700 SRM 51-24-16-001-001-A01, SRM 51-24-36-001-001-A01, SRM 51-40-11-001-001-A01.
Part: FRAME — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
F.S. 349 STR 26L-25R CORRODED IN MULTIPLE PLACES REMOVED AND REPLACED FRAME PN SH670-31357-5 AT F.S.349
Part: ANGLE — NONE · airframe 34,783 hrs · 26,207 cycles
FABRICATION REQUIRED OF REINFORCEMENT JOINT ANGLE STA 310 & 349 PN SH670-31947-4. PART REQUIRED FOR MWC BARCODE HN00221783 S/N: 00795. LOCATED AND DRILLED REINFORCEMENT JOINT ANGLE STA 310 & 349 FOR EXAMPLE OF P/N SH670-31947-4 FROM 7075-0 0.040ÿ½ PO# 5-59801 REFERENCING DRW SH670-31947 REV. NC AND AS PER SAMPLE IAW CRJ700 SRM 51-24-16-001-001-A01, SRM 51-24-36-001-001-A01, SRM 51-40-11-001-001-A01.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
SPLICE AT FS477 STR21R IS CORRODED. REQUIRE EVALUATION. REMOVED DAMAGED SPLICE AT STR21R AND FS477 IAW CRJ700 SRM 51-42-06-001-001-A01. STRINGER SPLICE AT 21R AND FS477 HAS MORE THAN 50 PERCENT MATERIAL LOSS. NO DAMAGE LIMITS GIVEN FOR SPLICE AT FS477 AND 21R. REQUIRES REPLACEMENT. LOCATED AND DRILLED NEW SERVICEABLE SPLICE P/N SH670-33252-1 AT STR21R & FS477 IAW CRJ700 SRM 51-40-11-001-001-A01.
Part: FRAME — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
FRAME SEGMENT AT FS333.00 CORRODED ON ATTACHED FLANGE AND FORWARD SIDE OF WEB BETWEEN STR 24R AND STR 26R. F.S. 333 FRAME SECTION AT STGR 24R - STGR 26R FOUND TO BE CORRODED BEYOND LIMITS IAW CRJ-700 SRM 53-00-06-201-005-A01. REMOVED CORRODED SECTION OF FRAME AND INSTALLED NEW SERVICEABLE F.S. 333 FRAME P/N SH670-31356-5 VIA SPLICE REPAIR AT STGR 25L TO FACTORY SPLICE AT STGR 20R IAW CRJ-700 SRM 53-00-06-201-006-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
STRG 23R (P/N SH670-31211-4) FOUND TO BE CORRODED BETWEEN FS295 - FS333. UPON FURTHER INVESTIGATION FOUND STR 23R BETWEEN FS280 - FS333 TO BE OUT OF LIMITS DUE TO EXCESSIVE CORROSION ON MORE THAN ONE ELEMENT OF STR 23R BETWEEN FS280 - FS333 IAW CRJ700 SRM 53-21-03-101-002-A01. REMOVED ALL FASTENERS TO UNSERVICEABLE STGR 23R (P/N:SH670-31211-4) BETWEEN FS280 - FS333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. REMOVED UNSERVICEABLE STGR 23R (P/N:SH670-31211-4) BETWEEN FS280 - FS333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. INSTALLED SAME SERVICEABLE 1EACH STANDOFF AT STGR 23R BETWEEN FS295-FS310 IAW CRJ 700 SRM 51-42-13-001-001-A01. INSTALLED SAME SERVICEABLE 2EACH STANDOFFS AT STGR 23R BETWEEN FS319-FS333 IAW CRJ 700 SRM 51-42-13-001-001-A01. INSTALLED SAME SERVICEABLE 3EACH CLEATS AT STGR 23R FS295,FS310 AND FS319 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE STGR 23R FS280-FS333 (P/N:SH670-31211-4U) IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE STGR 23R (P/N:SH670-31211-4U) BETWEEN FS280 - FS333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. EDGE SEALED AND PAINTED FASTENERS ON NEW SERVICEABLE STGR 23R BETWEEN FS280-FS333 (P/N:SH670-31211-4U) IAW CRJ700 SRM 51-23-00-001-001-A01 AND CRJ700 SRM 51-21-16-001-001-A01.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
"BTW FS .446 - 453 STGR 21R AND SPLICE IS CORRODED. REQUEST EVALUATION. UPON FURTHER INVESTIGATION CORROSION FOUND ON ST21R BETWEEN FS469 AND FS477 NO DAMAGE IS ALLOWED IN THIS SECTION OF THE STRINGER AS PER CRJ700 SRM 53-21-03-101-006-A01. REQUIRE REPLACEMENT OR REPAIR. SPLICE AT FS477 REQUIRE EVALUATION. THIS WORK WILL BE DONE WITH THE JOB CARD HN00233371 S/N 1168. PERFORMED CUT OUT AND REMOVED STR21R DAMAGED BETWEEN FS453 AND FS477 IAW CRJ700 SRM 53-00-03-201-001-A01 STEPS 5.A. (1) AND (2). PERFORMED HFEC OF STRINGER 21R FS453-FS477 CUTLINE EDGE IAW CRJ 700 NDTM PART 1 51-20-006-250-A01. NO INDICATIONS NOTED AT THIS TIME. FABRICATED, LOCATED AND DRILLED STR21R SECTION BETWEEN FS453 AND FS477 MATERIAL USED B0530021BF P.O.# 5-5689, STRINGER SPLICE ITEM 46 FROM B0530021BF P.O.# 5-5689 AND SHIM ITEM 47 FROM 2024T3 0.050"" P.O.# 5-22986 IAW CRJ700 SRM 53-00-03-201-001-A01 STEP 5.A. (4) TO (13). SOLUTION 2 FIG. 53-00-03-991-804 (SHEET 2 OF 3). INSTALLED REPAIR PARTS AT STR21R BETWEEN FS453 AND FS477 IAW CRJ700 SRM 53-00-03-201-001-A01 STEP 5.A (14) TO 6.A. APPLIED PAINT O INTERNAL FASTENERS IAW CRJ700 SRM 51-25-16-001-001-A01."
Part: STRINGER — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
STRG 23R (P/N SH670-31211-4) FOUND TO BE CORRODED BETWEEN FS295 - FS333. UPON FURTHER INVESTIGATION FOUND STR 23R BETWEEN FS280 - FS333 TO BE OUT OF LIMITS DUE TO EXCESSIVE CORROSION ON MORE THAN ONE ELEMENT OF STR 23R BETWEEN FS280 - FS333 IAW CRJ700 SRM 53-21-03-101-002-A01. REMOVED ALL FASTENERS TO UNSERVICEABLE STGR 23R (P/N:SH670-31211-4) BETWEEN FS280 - FS333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. REMOVED UNSERVICEABLE STGR 23R (P/N:SH670-31211-4) BETWEEN FS280 - FS333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. INSTALLED SAME SERVICEABLE 1EACH STANDOFF AT STGR 23R BETWEEN FS295-FS310 IAW CRJ 700 SRM 51-42-13-001-001-A01. INSTALLED SAME SERVICEABLE 2EACH STANDOFFS AT STGR 23R BETWEEN FS319-FS333 IAW CRJ 700 SRM 51-42-13-001-001-A01. INSTALLED SAME SERVICEABLE 3EACH CLEATS AT STGR 23R FS295,FS310 AND FS319 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE STGR 23R FS280-FS333 (P/N:SH670-31211-4U) IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE STGR 23R (P/N:SH670-31211-4U) BETWEEN FS280 - FS333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. EDGE SEALED AND PAINTED FASTENERS ON NEW SERVICEABLE STGR 23R BETWEEN FS280-FS333 (P/N:SH670-31211-4U) IAW CRJ700 SRM 51-23-00-001-001-A01 AND CRJ700 SRM 51-21-16-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
AT FS 370.00 STGR 20R IS CORRODED. REQUEST EVALUATION. REMOVED AND REPLACED STRINGER 20R (P/N SH670-31405-2) BTW FS 349 TO 477 IAW CRJ700 SRM 51-40-11-001-001-A01.DRILLED NEW STRINGER (P/N SH670-31405-2) BTW FS 364 TO FS 477 IAW CRJ700 SRM 51-40-11-001-001-A01 INSTALLED NEW STRINGER (P/N SH670-31405-2) BTW FS 364 TO FS 477 IAW CRJ700 SRM 51-40-11-001-001-A01
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
STGR 23R JOINT PIECE (SPLICE) AT FS333 FOUND TO BE CORRODED INSTALLED NEW SERVICEABLE STGR 23R JOINT PIECE SPLICE (P/N:SH670-32429-4S) AT FS333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01.
Part: ANGLE — CORRODED (ZONE 200) · airframe 34,783 hrs · 26,207 cycles
CLIPS ON FWD AND AFT FORMERS @ FS 320 AND 338 ARE CORRODED AND REQUIRE REPLACEMENT. REMOVED 4 EACH CORRODED CLIPS. LOCATED, DRILLED AND INSTALLED NEW CLIPS, 2 EACH P/N: 600-31902-275 AND 600-31902-276, IAW CRJ 700/900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV. 38 DATED JUL/25/2020.
Part: DOOR SILL — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
FORWARD CARGO DOOR SURROUND SILL P/N SH670-33764-3 AT STGR 25L IS CORRODED ON SILL TO FUSELAGE SKIN MATING SURFACE AT APPROX. FS526.00. REPAIRED IAW MHIRJ REO 670-53-31-1029 REV -- DATED 2025-04-25.
Part: SKIN — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
FOUND CORROSION ON INNER SKIN AROUND WHAT APPEARS TO BE A SKIN PLUG RIVET AT APPROXIMATELY F.S. 286 BETWEEN STGR 26R AND STGR 25R. REPAIRED IAW ENDEAVOR AIR EA NO: CRJ753-18599 REV. IR DATED 3/11/2025.
Part: STRINGER — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
STRG 24R (P/N SH670-31212-2) FOUND TO BE CORRODED BETWEEN FS295 - FS333. INSTALLED NEW STGR 24R P/N: SH670-31212-2 IAW CRJ700 SRM 51-42-06-001-001-A01. AND CRJ700 SRM 51-42-21-001-001-A01.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR LWR MID INTERCOSTAL DD7A IS CORRODED. REMOVED CORRODED PAX DOOR LWR MID INTERCOSTAL DD7. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318083-1, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020.
Part: ANGLE — CRACKED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR PRESSURE VENT FLAP ANGLE IS CRACKED. REMOVED CRACKED PAX DOOR PRESSURE VENT FLAP ANGLE. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R319055-1, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR AFT MID-LWR INTERCOSTAL IS CORRODED/DENTED. REMOVED CORRODED PAX DOOR AFT MID-LWR INTERCOSTAL. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R31902-317, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR AFT UPPER INTERCOSTAL DD1 IS CORRODED/DENTED. REMOVED CORRODED/DENTED PAX DOOR AFT UPPER INTERCOSTAL DD1. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R31902-318, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020.
Part: FORMER — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR AFT FORMER IS CORRODED. REMOVED CORRODED PAX DOOR AFT FORMER. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318034-5S, IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01,51-42-10-001-001-A01 AND 51-42-21-001-001-A01 REV. 38 DATED JUL 25/2020.
Part: HINGE — CHAFED (ZONE 200) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR HINGE AFT FLATS ARE CHAFED. REPAIRED CHAFE DAMAGE TO HINGE LUG LANDS (9) AFT END PAX DOOR HINGE IAW CRJ 700/900 SRM 52-11-01-201-007-A01 D. TYPE IV REV. 38 DATED JUL/25/2020. SEE CRJ 700/900 SRM 52-11-01-210-007-A01 2.A REQUIRES REINSPECT AT INTERVALS OF 5700 FLIGHT CYCLES IAW ND PART 1 CHAPTER 51-20-009 FOR CRACK IN LUG OR LUG FAILURE.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR AFT MID INTERCOSTAL CORRODED. REMOVED CORRODED PAX DOOR AFT MID INTERCOSTAL. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R31902-317A, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020.
Part: BRACKET — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR DD1A AFT BRACKET FOUND TO BE CRACKED. REMOVED PAX DOOR DD1A BRACKET. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318084-2, IAW CRJ 700/900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL/25/2020.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR LWR AFT INTERCOSTAL DD7 IS CORRODED/DENTED. REMOVED CORRODED PAX DOOR LWR AFT INTERCOSTAL DD7. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318825-1, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
JOINT PLATE, LOWER EXTERNAL P/N: SH670-33793-4 FS.533, STGR 25L IS HEAVY CORRODED INSTALLED NEW SERVICEABLE JOINT PLATE (PN: SH670-33793-4) IAW CRJ-700 SRM 51-42-22-001-001-A01, AND CRJ-700 SRM 51-42-21-001-001-A01.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
JOINT PLATE, LOWER EXTERNAL P/N: SH670-33793-3 FS.581, STGR 25L IS HEAVY CORRODED. INSTALLED NEW SERVICEABLE JOINT PLATE (PN: SH670-33793-3) IAW CRJ-700 SRM 51-42-22-001-001-A01, AND CRJ-700 SRM 51-42-21-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
STRG 22R (P/N SH670-31210-2) FOUND TO BE CORRODED BETWEEN FS280 - FS295. REMOVED STGR 22R P/N:SH670-31210-2 SEGMENT FROM FS 280.00 AND FS 333.00 IAW CRJ700 SRM 51-42-06-001-001-A01. AND CRJ700 SRM 51-42-21-001-001-A01. LOCATED AND DRILLED NEW STGR 22R P/N:SH670-31210-2U SEGMENT FROM FS 280.00 AND FS 333.00 IAW CRJ700 SRM 51-40-11-001-001-A01.INSTALLED NEW STGR 22R P/N:SH670-31210-2 SEGMENT FROM FS 280.00 AND FS 333.00 IAW CRJ700 SRM 51-42-06-001-001-A01. AND CRJ700 SRM 51-42-21-001-001-A01.EDGE SEALED AND PAINTED NEW STGR 22R IAW CRJ700 SRM 51-23-00-001-001-A01. AND CRJ700 SRM 51-21-16-001-001-A01.
Part: SKIN — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
FOUND CORROSION ON INNER SKIN AROUND WHAT APPEARS TO BE A SKIN PLUG RIVET AT APPROXIMATELY F.S. 286 BETWEEN STGR 26R AND STGR 25R. RECEIVED AND COMPLIED ALL STEPS OF OF ENDEAVOR AIR EA NO: CRJ753-18599 REV. IR DATED 3/11/2025.
Part: TIE DOWN — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
FS 530 AT STGR 27L CARGO TIE DOWN PAD IS CORRODED. REMOVED CORRODED CARGO TIE DOWN BRACKET AT FS 530 STGR 27 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED A SERVICEABLE RH CARGO TIE DOWN BRACKET (SH670-33369-1) AT FS 530 STGR 27 IAW CRJ 700 SRM 51-42-21-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 34,783 hrs · 26,207 cycles
LBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 1000 TO F.S. 1047. REMOVED LBL9 FLOOR SEAT TRACK BETWEEN F.S. 1000 TO F.S. 1047 INSTALLED LBL9 FLOOR SEAT TRACK BETWEEN F.S. 1000 TO F.S. 1047 IAW CRJ-700 53-00-49-400-802 (CONFIG A06).
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
INTERCOSTALS LEFT AND RIGHT OF STR 27 CORRODED F.S. 349-364, MARKED REMOVED CORROSION ON INTERCOSTALS LEFT (P/N SH670-32075-3) AND RIGHT (P/N SH670-32075-4) OF STGR 27 AT FS364. OUT OF LIMITS DUE TO MULTIPLE FACTORS INCLUDING DAMAGE COVERING MORE THAN 30 PERCENT OF INTERCOSTALS AND DAMAGE WITHIN 2D OF MULTIPLE FASTENER HOLES. INSTALLED NEW SERVICEABLE INTERCOSTAL RH P/N SH670-32075-4S AND INTERCOSTAL LH P/N SH670-32075-3S IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REMOVED AND INSTALLED 15EA SKIN RIVETS FROM L/H INTERCOSTAL AT STGR 27 AT FS364 IAW CRJ-700 SRM 51-42-06-001-001-A01. REMOVED AND INSTALLED 8EA HILITES FROM L/H INTERCOSTAL AT STGR 27 BETWEEN F.S. 349 AND F.S. 364 IAW CRJ-700 SRM 51-42-31-001-001-A01. REMOVED AND INSTALLED 15EA SKIN RIVETS FROM R/H INTERCOSTAL AT STGR 27 AT FS364 IAW CRJ-700 SRM 51-42-06-001-001-A01. REMOVED AND INSTALLED 8EA HILITES FROM R/H INTERCOSTAL AT STGR 27 BETWEEN F.S. 349 AND F.S. 364 IAW CRJ-700 SRM 51-42-31-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE INTERCOSTAL RH P/N SH670-32075-4S AND INTERCOSTAL LH P/N SH670-32075-3S IAW CRJ700 SRM 51-40-11-001-001-A01. DISCONNECTED AND RECONNECTED PROX SENSOR PX41 AT SPLICE IAW ESPM 20-44-00. PERFORMED OPS TEST OF THE MAIN AVIONICS COMPARTMENT DOOR (PX41) IAW CRJ700 AMM 52-42-00-710-801-A01. TEST PASSED. REMOVED AND INSTALLED 2EA PROX SENSOR (PX41) BRACKETS (P/N SH670-32106-1) FROM L/H AND R/H INTERCOSTALS IAW CRJ-700 SRM 51-42-21-001-001-A01. RESTORED SURFACE FINISH ON FASTENERS AT STGR 27 BETWEEN F.S. 349 - F.S. 364 IAW CRJ-700 SRM 51-25-16-001-001-A01. APPLIED CIC TO REPAIR AREA AT STGR 27 BETWEEN F.S. 349 - F.S. 364 IAW CRJ-700 SRM 51-21-11-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
APPROX F.S.370 STR 21R SEVERELY CORRODED AT FASTENER HOLE (F.S. 364-379), MARKED LOCATED AND DRILLED NEW SERVICEABLE STR 21R PN: SH670-31383-1S AT FS333 TO FS394 IAW CRJ700 SRM 51-40-11-001-001-A01.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 34,783 hrs · 26,207 cycles
RBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 1000 TO F.S. 1047. REMOVED RBL9 FLOOR SEAT TRACK BETWEEN F.S. 1000 TO F.S. 1047 INSTALLED RBL9 FLOOR SEAT TRACK BETWEEN F.S. 1000 TO F.S. 1047 IAW CRJ-700 53-00-49-400-802 (CONFIG A06).
Part: STRINGER — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
STR 26R F.S. 310-364 CORRODED IN MULTIPLE PLACES, MARKED. LOCATED AND DRILLED SERVICEABLE STGR 26R (P/N: SH670-31634-2S) IAW CRJ 700 SRM 51-40-11-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE STGR 26R AFT (P/N: SH670-31372-4S) IAW CRJ-700 SRM 51-40-11-001-001-A01. INSTALLED STGR 26R BETWEEN FS 280 - FS 333 IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE STGR 26R BETWEEN FS 333 - FS 364 IAW CRJ 700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED SAME SERVICEABLE STGR 26R SPLICE @ FS333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01.
Part: FRAME — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
F.S. 295 STR 26L-26R CORRODED ON FWD AND AFT SIDE OF FRAME. REPAIRED BY CUTTING AWAY DAMAGED SECTION AND SPLICING IN REPAIR PARTS IAW CRJ700 SRM 53-00-06-201-006-A01.
Part: FRAME — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
FS 319 FRAME IS CORRODED BETWEEN STRINGERS 26L-26R. CUT AWAY DAMAGED PORTION OF FRAME AND SPLICED IN REPAIR PARTS IAW CRJ 700 SRM 53-00-06-201-006-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
F.S. 280-310 STR 25R CORRODED. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 34,783 hrs · 26,207 cycles
F.S. 280-295 STR 26L CORRODED. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 34,783 hrs · 26,207 cycles
FS280 RH FLOOR SUPPORT HAS CORROSION BETWEEN RBL9 AND FLOOR SILL IN 2EA LOCATIONS. REMOVED DAMAGED FS 280.00 RH CROSSBEAM IAW CRJ700 SRM 51-42-06-001-001-A01. CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-42-13-001-001-A01. LOCATED AND DRILLED NEW RH FS.280 FLOOR BEAM PN# CC670-34175-7 IAW CRJ-700 SRM 51-40-11-001-001-A01 INSTALLED NEW SERVICEABLE FS280.00 RH CROSSBEAM (P/N:CC670-34175-7) IAW CRJ700 SRM 51-42-06-001-001-A01,CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-42-13-001-001-A01.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR INTERCOSTAL AT DD3 CORRODED. REMOVED CORRODED INTERCOSTAL DD3. LOCATED, DRILLED, AND INSTALLED NEW PART, P/N: 601R318056-1, IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01 REV 38 DATED 25 JUL 2020.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR LWR MID INTERCOSTAL DD6 IS CORRODED. REMOVED CORRODED PAX DOOR LWR MID INTERCOSTAL DD6. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318057-1, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020.
Part: FORMER — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR FWD FORMER AT APPROX FS311.75 CORRODED. REMOVED CORRODED FWD FORMER. LOCATED, DRILLED, AND INSTALLED NEW PART, P/N 601R318031-5S, IAW CRJ 700/900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01 REV 38 DATED JUL 25/2020
Part: FORMER — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR MID FORMER, F.S.349.41, DD4/DD5 IS CORRODED. REMOVED CORRODED PAX DOOR MID FORMER, F.S. 349.41, DD4/DD5. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318078-3, IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV. 38 DATED JUL 25/2020.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR LWR FWD INTERCOSTAL DD7 IS CORRODED/DENTED. REMOVED CORRODED/DENTED PAX DOOR LWR FWD INTERCOSTAL DD7. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318826-1, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED 25 JUL 2020.
Part: DOOR FRAME — CORRODED (ZONE 200) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR FORMER AT FS320.163 CORRODED BETWEEN DD4 AND DD5. REMOVED CORRODED FRAME AT F.S. 320-163. LOCATED, DRILLED, AND INSTALLED NEW PART, P/N: 601R318032-5, IAW CRJ 700/900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01 REV. 38 DATED JUL/25/2020.
Part: ANGLE — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR OUTER HANDLE LWR SUPPORT ANGLE IS CORRODED. REMOVED CORRODED PAX DOOR OUTER HANDLE LWR SUPPORT ANGLE. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R317052-1, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01 REV. 38 DATED JUL 25/2020.
Part: FORMER — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR MID FORMER, F.S.329.41, DD5/DD6 IS CORRODED. REMOVED CORRODED PAX DOOR MID FORMER, F.S. 329.41, DD5/DD6. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318078-3, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED JUL 25/2020.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR MID INTERCOSTAL DD4 IS CORRODED. REMOVED CORRODED PAX DOOR MID INTERCOSTAL DD4. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318081-15, IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV. 38 DATED JUL 25/2020.
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR FWD MID INTERCOSTAL DD3 IS CORRODED/DENTED. REMOVED CORRODED/DENTED FWD MID INTERCOSTAL DD3. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318054-1, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED 25 JUL 2020
Part: INTERCOSTAL — CORRODED (ZONE 800) · airframe 34,783 hrs · 26,207 cycles
PAX DOOR MID UPPER INTERCOSTAL DD2 IS CORRODED. REMOVED CORRODED PAX DOOR MID UPPER INTERCOSTAL DD2. LOCATED, DRILLED AND INSTALLED NEW PART, P/N: 601R318053-3, IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REV. 38 DATED 25 JUL 2020.
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 34,779 hrs · 26,206 cycles
BOTH EMERGENCY LIGHT BULBS INOP ON FUSELAGE EXTERIOR RH SIDE, OVERWING AND AFT LOCATIONS. R/R BOTH EMERGENCY LIGHT BULBS INOP ON FUSELAGE EXTERIOR RH SIDE IAW AMM 33-51-15. OPS CHECK GOOD. P/N OFF/ON:8GH002473-08
Earlier reports · 2005–2023 · 98 reports
2023
Part: BRACKET — CRACKED · airframe 34,777 hrs · 26,205 cycles
PAX DOOR ASSIST MOTOR CABLE YOKE BRACKET CRACKED REMOVED AND REPLACED BRACKET
2019
Part: WEB — CRACKED (FUSELAGE) · airframe 33,404 hrs · 24,886 cycles
RT FLOOR WEB CRACKED IN NOSE EQUIPMENT COMPARTMENT NEAR ADG PUMP. CORRECTIVE ACTION: REPAIRED RT FLOOR WEB BY CUTTING DAMAGED AREA AND INSTALLED REPAIR PARTS IAW REO 670-53-11-1530 DATED 2019-06-13, REO 670-53-11-509 REV. E DATED 2018-02-08, AMM 20-70-00 AND SRM 51-42-06.
Part: SKIN — CORRODED (BS 939-953) · airframe 33,404 hrs · 24,886 cycles
MULTIPLE FASTENERS ON EXTERNAL SKIN AT F.S. 939 TO F.S. 953 STGR 20R-25R AND AT STGR 27 HAVE SIGNS OF CORROSION. CLEANED, EVALUATED, AND REPAIRED AREAS WITH CORROSION AND REPLACED FASTENERS IAW BOMBARDIER REO 670-53-51-146 DATED 2019-06-15.
Part: TRIPLER — GOUGED (BS 977) · airframe 33,404 hrs · 24,886 cycles
TRIPLER REPAIR AT F.S. 977.00 STGR 27 IS GOUGED. REMOVED EXISTING REPAIR AND FABRICATED NEW REPAIR PARTS AND INSTALLED THEM IAW REO 670-53-00-290 REV-F, AND DWG PL BA670-39313 REV-A.
2018
Part: UNKNOWN — ODOR (CABIN) · airframe 32,305 hrs · 23,861 cycles
SMELL OF SMOKE IN CABIN. PERFORM OPS CHECK OF AIR DIST IAW CRJ 700AMM 21-51-00 NO SMOKE NOTED MXC NOTIFIED OK FOR SERVICE INSPECTED A/C CABIN COPIT FUSELAGE ACM EXHUAST PARTS NO ODOR OR SIGN OF SMOKE
Part: FRAME — CORRODED (FUSELAGE) · airframe 31,425 hrs · 23,051 cycles
FRAME SECTION AT FS 319.00 SHOWS SIGNS OF CORROSION AT STR 21L. REMOVED AND REPLACED FRAME SECTION AT FS 319.00 AND STR 21L IAW SRM 51-42-06, 51-40-11, 53-21-23, 51-25-16, 51-21-11
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,425 hrs · 23,051 cycles
INTERCOSTAL AT STR 21 L BETWEEN FS 310-349 HAS SIGNS OF CORROSION. REMOVED AND REPLACED INTERCOSTAL BETWEEN FS 310-349 IAW SRM 51-42-06, 53-21-23, 51-40-11, 51-42-21, 51-40-11, 51-25-16, 51-21-11 AND AMM 25-82-01, 25-84-00 AND NDTM PART 1 51-20-006 AND REO 670-53-21 1538 REV -- DATED 2018-07-06
Part: WEB — CORRODED (FUSELAGE) · airframe 31,425 hrs · 23,051 cycles
RT LOWER WEB AT FS 280 BULKHEAD CORRODED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-42-13, 51-42-06, 51-25-16, 51-25-06, 51-21-11 AND REO 670-53-11-594 REV -- DATED 2011-04-24.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 31,425 hrs · 23,051 cycles
RT FS 280 LOWER WEB CORRODED. REPLACED RT FS 280 BULKHEAD LOWER WEB IAW REO 670-53-11-594 REV- DATED 2011-04-27 AND SRM 51-42-13, 51-42-06, 51-25-16, 51-25-06, 51-21-11,
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 31,425 hrs · 23,051 cycles
RT FLOOR SILL AT FS 280 HAS CORROSION. REPAIRED RT FLOOR SILL AT FS 280 IAW REO 670-53-00-390 REV- DATED 22/JAN/2014 AND NDTM PART 1 51-20-006 AND SRM 53-00-00.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 31,425 hrs · 23,051 cycles
RT FLOOR SILL HAS CORROSION BETWEEN FS 349 AND FS 379. REPAIRED RT FLOOR SILL BETWEEN FS 349 AND FS 379 IAW REO 670-53-00-390 REV- DATED 22 JAN 2014 AND NDTM PART 1 51-20-006.
Part: DOUBLER — CRACKED (PAX DOOR) · airframe 31,425 hrs · 23,051 cycles
PASSENGER DOOR INTERNAL DOUBLER UNDER PANEL 832AR IS CRACKED. REPLACED DOUBLER IAW SRM 51-46-02, 51-40-11, 51-42-13, 51-42-21.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 31,425 hrs · 23,051 cycles
T STR 21L BETWEEN FS 310-333 HAS SIGNS OF CORROSION. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW REO 670-53-21-1536 DATED 2018-06-30 AND SRM 53-21-03 AND NDTM PART 01 51-20-006.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 31,425 hrs · 23,051 cycles
INTERCOSTAL AT STRINGER 20R BETWEEN FS 310 AND 319 CORRODED OUT OF LIMITS IAW SRM 53-21-23. REPLACED INTERCOSTAL BETWEEN FS 310 AND 319 IAW SRM 51-40-11, 51-25-06, 51-25-16, 51-21-11 AND AMM 25-82-01.
Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 31,425 hrs · 23,051 cycles
GALLEY SERVICE DOOR KICK ANGLE CORRODED. REPLACED GALLEY SERVICE DOOR KICK ANGLE IAW SRM 51-42-21, 51-42-06, 53-21-27, 53-21-23, 51-40-11, 53-21-27, 51-25-21, 51-26-00, 51-21-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,425 hrs · 23,051 cycles
TWO RT FLOOR SEAT RAILS BETWEEN FS 485 AND FS 677 ARE CORRODED. EVALUATED CORRODED SEAT RAILS IAW REO 670-53-00-013 REV J DATED 2014/10/22 AND SRM 53-31-49. FOUND CORROSION TO BE OUT OF LIMITS. REPLACED 2 CORRODED SEAT RAILS IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 31,425 hrs · 23,051 cycles
TWO LT FLOOR SEAT RAILS BETWEEN FS 485 AND FS 677 ARE CORRODED. EVALUATED CORRODED SEAT RAILS IAW REO 670-53-00-013 REV J DATED 2014/10/22 AND SRM 53-31-49. FOUND CORROSION TO BE OUT OF LIMITS. REPLACED 2 CORRODED SEAT RAILS IAW AMM 53-00-49.
Part: STIFFENER — CRACKED (PAX DOOR) · airframe 31,425 hrs · 23,051 cycles
PASSENGER DOOR POWER ASSIST MOTOR MOUNT BRACKET (STIFFENER) CRACKED. REPLACED POWER ASSIST MOTOR MOUNT BRACKET (STIFFENER) IAW SRM 51-42-06 AND 51-42-13.
Part: BEAM — CRACKED (FUSELAGE) · airframe 31,425 hrs · 23,051 cycles
RT FS 280.00 BEAM HAS A CRACK. REMOVED AND REPLACED RT 280 BEAM IAW SRM 53-11-41, 51-42-13, 51-24-36, 51-42-06, 51-42-21, 51-40-11, 51-25-06, 51-21-10, 51-25-16, 53-11-10, AND AMM 20-70-00.
2017
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 29,015 hrs · 20,838 cycles
FWD SIDE OF BULKHEAD AT FS 202.75 FOUND AN INDICATION ON TOP OF STIFFENER LBL30 APPROX 1/4" L. FAILED NDT INSPECTION.
2016
Part: DRAG ANGLE — CRACKED (VERT TO FUSE) · airframe 28,431 hrs · 24,015 cycles
VERTICAL STABILIZER TO FUSELAGE, LT FWD DRAG ANGLE IS CRACKED.. CUT OUT DAMAGE, FABRICATED AND INSTALLED A REPAIR IAW REO 670-53-31-018.
Part: SEAT TRACK — CORRODED (BS 581-613) · airframe 28,431 hrs · 24,015 cycles
SEAT TRACK BETWEEN BS 581 AND 613 CORRODED. REPLACED THE LT SIDE SEAT TRACK IAW AMM 53-0049 AND 20-21-00.
Part: SEAT TRACK — CORRODED (BS 597-629) · airframe 28,431 hrs · 24,015 cycles
SEAT TRACK BETWEEN BS 597 AND 629 CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-00-49 AND 20-21-00.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,431 hrs · 24,015 cycles
REPLACE LT SIDE SEAT RAIL BETWEEN FS 843.00 AND FS 923.00. REPLACED LT SIDE SEAT RAIL BETWEEN FS 843.00 AND FS 923.00 IAW AMM 53-00-49 AND 20-21-00, AND SB670BA-25-094 REV E, DATED AUG 05 2016.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,431 hrs · 24,015 cycles
REPLACE LT SIDE SEAT RAIL BETWEEN FS 939.0 AND 953.00. REPLACED LT SEAT TRACK BETWEEN FS 939.00 AND 953.00 IAW AMM 53-00-49 AND 20-21-00 AND SB 670BA-25-094 REVISION E DATED AUG 5, 2015.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 28,431 hrs · 24,015 cycles
REPLACE LT SIDE SEAT RAIL BETWEEN FS 797.00 AND FS 847.00. REMOVED AND REPLACED LT SIDE SEAT TRACK BETWEEN FS 797.00 AND 847.00 IAW AMM 53-00-49 AND SB 670BA-25-094 REV E, DATED AUG 5, 2015.
Part: SEAT TRACK — CORRODED (BS 485-533) · airframe 28,431 hrs · 24,015 cycles
SEAT TRACK BETWEEN BS 485 - 533 CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-00-49 AND 20-21-00.
Part: SEAT TRACK — CORRODED (BS 549-565) · airframe 28,431 hrs · 24,015 cycles
RIGHT SIDE SEAT TRACK BETWEEN BS 549 - 565 CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-00-49, AND 20-21-00.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,431 hrs · 24,015 cycles
AFT CARGO DOOR SILL CORRODED OUT OF LIMITS. REMOVED AND REPLACED AFT CARGO DOOR SILL IAW SRM 51-42-06, 51-42-10, 51-40-11, 51-42-21. 51-41-02, AND 51-21-16
Part: DOOR — GOUGED (RT NACELLE) · airframe 28,431 hrs · 24,015 cycles
RIGHT ENGINE NACELLE BLOWOFF DOOR STRIKER PLATE GOUGED OUT OF LIMITS. REMOVED AND INSTALLED A NEW NACELLE BLOW OFF DOOR STRIKER PLATE IAW SRM 51-42-13, AND SRM 51-42-06.
Part: CAP — CORRODED (FUSELAGE) · airframe 28,431 hrs · 24,015 cycles
PAX DOOR KICK ANGLE AND MIDCAP ARE CORRODED. INSTALLED NEW KICK ANGLE IAW SRM 51-42-06. INSTALLED NEW MIDCAP IAW SRM 51-41-00.
Part: DOUBLER — GOUGED (FUSELAGE) · airframe 28,431 hrs · 24,015 cycles
REPAIR DOUBLER ON LOWER AIRCRAFT EXTERNAL SKIN AT FRAME STATION 977.00 IS GOUGED IN THREE LOCATIONS. REMOVED AND REPLACED TOP DOUBLER, PRIMED, TOP COATED, AND CIC'D IAW REO 670-53-00-290 REV-D DATED 2015-09-10, SRM 51-25-06, AND 51-21-01.
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 28,431 hrs · 24,015 cycles
RT AFT DRAG ANGLE IS CRACKED WHERE VERTICAL STABILIZER MEETS FUSELAGE. REPAIRED RT AFT DRAG ANGLE IAW REO 670-55-31-018 REV A DATED 2016-11-10, AND REO 670-55-31-092 DATED 2016-12-06. NDT PERFORMED.
Part: HOUSING — GOUGED (CARGO DOOR) · airframe 28,431 hrs · 24,015 cycles
AFT CARGO DOOR EXTERNAL HANDLE HOUSING GOUGED OUT OF LIMITS IAW REO 670-52-31-031 REV-A DATED 2016-10-03. REPLACED AFT CARGO DOOR HANDLE HOUSING IAW SRM 51-42-21.
Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR LATCH) · airframe 27,726 hrs · 19,894 cycles
PASSENGER DOOR LATCH CAUTION MESSAGE. INSPECTED AND PERFORMED OPS CHECK OF PAX DOOR LATCH MECHANISM IAW AMM 52-11-07. OPS CHECKED GOOD, NO FAULTS OR CAUTION MESSAGES NOTED.
Part: WARNING MESSAGE — INTERMITTENT (PAX DOOR) · airframe 27,720 hrs · 19,889 cycles
PAX DOOR LATCH CAUTION MESSAGE INTERMITTENT DURING FLT.
Part: FLOORBEAM — CORRODED (BS 1031) · airframe 27,042 hrs · 19,383 cycles
FLOORBEAM BS 1031, RBL 9 ,WL 72 FOUND TO BE CORRODED BEYOND ALLOWABLE LIMITS. FLOORBEAM WAS REPAIRED IAW REO 670-53-00-029 REV A.
Part: FLOORBEAM — CORRODED (BS 1031) · airframe 27,042 hrs · 19,383 cycles
FLOORBEAM AT BS 1031, RBL, WL 72 FOUND TO BE CORRODED BEYOND ALLOWABLE LIMITS. FLOORBEAM REPAIRED IAW REO 670-53-00-029, REV A, DATED 08-31-2010.
2015
Part: DOOR SEAL — DAMAGED (PAX DOOR) · airframe 25,976 hrs · 18,568 cycles
LOUD NOISE COMING FROM MAIN PAX DOOR EN-ROUTE. INSPECTED DOOR SEAL, FOUND TEAR ON THE TOP PART OF THE DOOR SEAL. REPAIRED DOOR SEAL IAW SRM 52-11-07. PRESSURIZED ACFT IAW AMM 21-31-00. OPERATIONS CHECKED GOOD AT THIS TIME.
Part: DOOR SILL — DIRTY (FUSELAGE) · airframe 25,975 hrs · 18,566 cycles
PASSENGER DOOR MAKES SQUEALING SOUNDS IN FLIGHT. REMOVED DEBRIS FROM PAX DOOR SILL AREA. PERFORMED PRESSURIZATION CHECK IAW AMM 21-31-00, NO DEFECTS NOTED AT THIS TIME.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 24,996 hrs · 17,829 cycles
LEFT EMER DOOR CAUTION. DEFERRED LT EMER DOOR INDICATION INTERMITTENT IAW MEL 52-70-03 CAT C.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 24,990 hrs · 17,823 cycles
LEFT EMER DOOR CAUTION INTERMITTENT. DEFERRED EMER EXIT DOOR CAUTION MSG IAW MEL 52-70-03 CAT C.
Part: WHEEL — MALFUNCTIONED (PAX DOOR) · airframe 24,709 hrs · 17,615 cycles
PASSENGER DOOR WHEEL DID NOT DEPLOY. INSPECTED PAX DOOR FOR STRUCTURAL DAMAGE, NONE NOTED. ACFT SAFE FOR A ONE TIME FERRY FLIGHT.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 24,444 hrs · 17,423 cycles
LEFT OVERWING EMER EXIT CAUTION MSG. DEFERRED LT OVERWING EXIT CAUTION MSG IAW MEL 52-70-03 CAT C.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 24,436 hrs · 17,417 cycles
LEFT EMER DOOR CAUTION MSG AFTER LANDING. COMPLIED WITH LT EMER DOOR CAUTION MSG IAW AMM 52-21-00. NO MSGS NOTED ON OPERATIONS CHECK.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 24,384 hrs · 17,374 cycles
INBOARD LT INTERCOSTAL FWD OF FS 364 CORRODED IN AVIONICS BAY. R & R INBD LT INTERCOSTAL FWD OF FS 364 IN AVIONICS BAY IAW SRM 51-42-06 & 51-42-21.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 24,384 hrs · 17,374 cycles
MAIN AVIONICS BAY STRINGER 25R AT FS 328 & SPLICE CORRODED. R & R STRINGER 25R AT FS 328 & SPLICE IAW REO 670-21-1158 DATE 2015-01-19. NDT PERFORMED INSPECTION SERVICES CRS K9QR55413, 1/21/2015, JOB AV0116158J, PO 124889, NO DEFECTS NOTED.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 24,384 hrs · 17,374 cycles
MAIN AVIONICS BAY STRINGER 26R AT FS 323 - 364 CORRODED. R & R STRINGER 26R AT FS 323 - 364 IAW REO 670-53-21-1156 DATE 2015-01-16. NDT PERFORMED INSPECTION SERVICES CRS K9QR55413, JOB AV0116158J, PO 124889, 01/21/2015, NO DEFECTS NOTED.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 24,384 hrs · 17,374 cycles
INBOARD RT INTERCOSTAL FWD OF FS 364 IN MAIN AVIONICS BAY CORRODED. R & R INBD RT INTERCOSTAL FWD OF FS 364 IN MAIN AVIONICS BAY IAW SRM 51-42-21 & 51-42-06.
Part: STRUCTURE — GOUGED (FUSELAGE) · airframe 24,384 hrs · 17,374 cycles
GOUGED IN FUSELAGE X3 AT STRINGER 27 FS 969. REPAIRED FUSELAGE AT STRINGER 27 FS 969 IAW REO 670-53-00-290. NDT PERFORMED INSPECTION K9QR554B DATE 1-19-2015, JOB AV0116158J, PO 124820, NO DEFECTS NOTED IAW REO 670-53-00-290 REV C 2013-03-21.
Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 24,384 hrs · 17,374 cycles
CROSSBEAM AT FS 280 LT & RT CRACKED & CORRODED. REMOVED CRACKED & CORRODED FS 280 CROSSBEAM & INSTALLED NEW FS CROSSBEAM IAW SRM 53-11-41. NDT PERFORMED ON 16 JAN 2015, CRS K9QR554B, JOB AV0116158J, PP 124820, NO RELEVANT INDICATION NOTED. SEE REPORT.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 24,384 hrs · 17,374 cycles
FORWARD 1/4 TURN FLOOR SUPPORT ANGLE AT FS 280 CORRODED. REMOVED CORRODED AFT 1/4 TURN FLOOR SUPPORT ANGLE AT FS 280 INSTALLED NEW 1/4 TURN ANGLE IAW SRM 51-42-06.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 24,384 hrs · 17,374 cycles
LEFT & RIGHT FS 280 LOWER BULKHEAD CORRODED WEB. CUT OUT & REMOVED CORRODED LT & RT LOWER WEBS & FABRICATED & INSTALLED REPAIR PARTS IAW REO 670-53-11-594 DATE 2011-04-27.
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 24,384 hrs · 17,374 cycles
T CAS ANTENNA CHANNEL IN MAIN AVIONICS BAY CORRODED. R & R T CAS ANTENNA DOUBLER IAW 51-42-06, 51-42-21 & 51-40-11.
2014
Part: UNKNOWN — SMOKE (CABIN) · airframe 24,216 hrs · 17,249 cycles
SMOKE COMING FROM COCKPIT VENTS WHEN PACKS TURNED ON. PERFORMED OPS CHECK OF PACKS IAW AMM 21-51-00. NO DEFECTS NOTED AT THIS TIME.
Part: COVER — DETACHED (EMERGENCY EXIT) · airframe 24,185 hrs · 17,225 cycles
RIGHT WING EMER EXIT COVER DETACHED. SECURED RT WING EMER EXIT COVER IAW AMM 51-22-00. NO DEFECTS NOTED AT THIS TIME.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,826 hrs · 16,966 cycles
EMERGENCY LIGHT AT CEILING ROW 8 INOPERATIVE. REPLACED BULB AT EMER LIGHT AT ROW 8 IAW AMM 33-51-09. OPERATIONS CHECKED GOOD.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 23,487 hrs · 16,705 cycles
PAX DOOR OUTER HANDLE CAUTION MSG. PERFORMED OPERATIONS CHECK OF PSEU FIM 32-60-00. NO MSG DISPLAYS, ACFT OK FOR SERVICE.
Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 16,014 hrs · 10,517 cycles
LEFT BLEED MASTER CAUTION WARNING IN FLIGHT. FOUND LOOSE CLAMP ON LT BLEED DUCT & FELT LEAK. TIGHTENED CLAMP & OPS CHECKED GOOD IAW AMM 36-21-00.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 23,335 hrs · 16,592 cycles
PAX DOOR OUTER HANDLE CAUTION MSG IN FLIGHT, IT WENT AWAY AFTER LANDING. OPERATIONS CHECKED PAX DOOR IAW AMM 52-11-03. OPERATIONS CHECKED GOOD AT THIS TIME, NO DEFECTS NOTED AT THIS TIME.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,828 hrs · 16,184 cycles
EMERGENCY LIGHT ABOVE PAX DOOR INOPERATIVE. R & R BULBS ABOVE PAX DOOR IAW AMM 33-51-05, OPERATIONS CHECKED GOOD.
Part: OIL SYSTEM — LOW (LT ENGINE) · airframe 22,559 hrs · 15,970 cycles
LEFT ENGINE OIL LOW. SERVICED ENGINE OIL IAW AMM 12-13-79, NO LEAKS NOTED AT THIS TIME.
Part: LIGHT — LOOSE (CABIN) · airframe 22,507 hrs · 15,930 cycles
PHOTO ILLUMINATION STRIP BY CLOSET AT ENTRY LOOSE. SECURED PHOTO ILLUMINATION STRIP IAW CRJ700 AMM 33-51-01. ACFT OK FOR SERVICE.
Part: PROXIMITY SENSOR — OUT OF ADJUST (LANDING GEAR) · airframe 22,027 hrs · 15,571 cycles
GEAR DISAGREE WARNING MESSAGE. INSPECTED & FOUND PX03 PROX SENSOR OUT OF ADJUSTMENT. ADJUSTED PXO3 IAW CRJ700 AMM 32-61-05. PERFORMED OPERATIONS LG PSS IAW CRJ700 AMM 32-61-00. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.
2013
Part: DOOR — UNSECURE (EMERGENCY EXIT) · airframe 21,611 hrs · 15,240 cycles
LEFT EMERGENCY LIGHT CYCLING ON AND OFF. ADJUSTED AND SECURED LT EMERGENCY EXIT DOOR IAW AMM 52-21-00, OPS AND LEAK CHECKED GOOD AT THIS TIME.
Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 21,594 hrs · 15,228 cycles
LEFT EMERGENCY DOOR CAUTION MESSAGE. LUBRICATED LT EMERGENCY DOOR IAW AMM 52-21-05, OPS CHECKED GOOD.
Part: WARNING LIGHT — UNKNOWN (EMERGENCY EXIT) · airframe 21,472 hrs · 15,130 cycles
LEFT EMERGENCY DOOR CAUTION AFTER LANDING. ADJUSTED DOOR TRIM, REMOVED & REINSTALLED DOOR AND PERFORMED ADJUSTED/TEST IAW 52-21-00. NO DEFECTS NOTED AT THIS TIME.
Part: WARNING MESSAGE — ILLUMINATED (EMERGENCY EXIT) · airframe 21,464 hrs · 15,125 cycles
LEFT EMERGENCY DOOR CAUTION MESSAGE.
Part: WARNING LIGHT — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 21,025 hrs · 14,773 cycles
LEFT EMERGENCY DOOR CAUTION MESSAGE. OP'S CHECKED LEFT EMERGENCY DOOR IAW AMM 52-21-00, OP'S CHECKED GOOD.
Part: LATCH — LACK OF LUBE (EMERGENCY EXIT) · airframe 20,714 hrs · 14,532 cycles
LEFT EMERGENCY DOOR CAUTION MESSAGE. CLEANED, LUBED LATCH ON LT EMERGENCY DOOR IAW AMM 52-21-00. OP'S CHECK GOOD.
Part: WARNING LIGHT — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 20,516 hrs · 14,387 cycles
LEFT EMERGENCY EXIT CAUTION MESSAGE ON LANDING. INSPECTED AND PERFORMED OP'S CHECK OF OVERWING EXIT IAW AMM 52-21-00, OP'S CHECKED GOOD AT THIS TIME.
Part: INDICATOR — INACCURATE (AIRSPEED) · airframe 20,405 hrs · 14,304 cycles
DURING TAKEOFF ROLL, PILOT NOTICED AIRSPEED SPLIT AT 100 KAIS. INSPECTED PITOT SYS WATER TRAPS, FOUND TO BE DRY. PERFORMED FUNCTIONAL CHECK OF NR1 AND NR2 AIR DATA SYSTEMS IAW AMM 34-13-01. NO DEFECTS NOTED, PERFORMED LEAK CHECK ON NR 1 AND NR 2 AIR DATA SYS IAW AMM 34-11-00. NO DEFECTS NOTED.
Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT) · airframe 20,400 hrs · 14,301 cycles
LEFT EMERGENCY DOOR CAUTION MESSAGE. PERFORMED ADJUSTMENT TEST OF PASSENGER DOOR WARNING SYS IAW AMM 52-70-04.
Part: WARNING MESSAGE — ILLUMINATED (EMERGENCY EXIT) · airframe 20,356 hrs · 14,270 cycles
LEFT EMERGENCY DOOR CAUTION MESSAGE ON TAKEOFF.
Part: COVER — UNSECURE (EMERGENCY DOOR) · airframe 20,106 hrs · 14,086 cycles
RIGHT EMERGENCY EXIT HANDLE COVER FELL OFF. SECURED RT EMERGENCY EXIT HANDLE COVER IAW AMM 52-21-02. OP'S CHECKED GOOD AT THIS TIME.
Part: CABLE — INOPERATIVE (PAX DOOR) · airframe 19,832 hrs · 13,880 cycles
PAX DOOR WILL NOT CLOSE. R & R PAX DOOR BOTTOM CABLE IAW 52-11-13, OP'S CHECKED GOOD AT THIS TIME.
2012
Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 19,558 hrs · 13,684 cycles
FLOOR EMERGENCY LIGHT COVER AT ROWS 9-11 LOOSE. RESECURED FLOOR EMERGENCY LIGHT COVER IAW AMM 33-51-01.
Part: SEAL — LEAKING (EMERGENCY EXIT) · airframe 19,370 hrs · 13,537 cycles
RT OVERWING EMERGENCY EXIT DOOR WAS WHISTLING IN FLIGHT. REMOVED HATCH DOOR AND CLEANED DEBRIS FROM SEAL AND DOOR JAM, LUBRICATED SEAL, REINSTALLED HATCH DOOR IAW AMM 52-21-00
Part: STRINGER — CRACKED (ZONE 200) · airframe 19,092 hrs · 13,331 cycles
LINTEL STRINGER 3L FS 280 OF MAIN PAX DOOR CRACKED. REPAIRED LINTEL STRINGER IAW SB 670BA-53-040 AND REO 670-53-21-493, REV C, RIL 2883, REV A.
Part: HINGE — CRACKED (PAX DOOR STEP) · airframe 19,092 hrs · 13,331 cycles
PAX DOOR TOP STEP HINGE CRACKED. R & R HINGE IAW SRM 51-41-02, 51-40-11, 51-21-11.
Part: SEAT TRACK — CORRODED (BS 693-827) · airframe 19,092 hrs · 13,331 cycles
RT SEAT TRACK HAS COROSION FS 693-827. R & R SEAT TRACK IAW REO 670-53-00-074 AND SRM 53-21-11, 53-41-49.
Part: STRINGER — CRACKED (ZONE 200) · airframe 19,092 hrs · 13,331 cycles
LINTEL STRINGER 3 LT MAIN PASSENGER DOOR IS CRACKED. REPAIRED LINTEL STR. 3 LT MAIN PASSENGER DOOR AS REQUIRED IAW SB670BA-53-040, REO 670-53-21-493, REV C, AND RIL 2883 REV A, NDT COMPLIED WITH.
Part: STRIKER — SCRATCHED (ZONE 200) · airframe 19,092 hrs · 13,331 cycles
LT SIDE STRIKER PLATE ON PASSENGER DOOR HAS A SCRATCH ABOUT 75 PERCENT OF THE WAY UP, THE ENTRANCE. BLENDED LT SIDE STRIKER PLATE ON PASSENGER DOOR IAW SRM 53-21-23. REMOVED 0.008 FROM STRIKER, THICKNESS 0.100 WITHIN 10 PERCENT LIMIT.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 19,092 hrs · 13,331 cycles
SEAT TRACK HAS COROSION AT FS 893 AND 923. REMOVED CORROSION FOUND TO BE WITH IN LIMITS IAW SRM 53-51-51, 51-25-06, 51-21-11.
2011
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 17,338 hrs · 12,050 cycles
PAX DOOR THRESHOLD ANGLE IS CORRODED. REMOVED AND REPLACED PAX DOOR THRESHOLD ANGLE P/N SH670-31825-9 IAW CRJ AMM 20-21-00 AND SRM 51-21-23.
Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 17,338 hrs · 12,050 cycles
RIGHT SIDE FS 280.00 CROSSBEAM IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FS 280.00 CROSSBEAM IAW REO 670-53-11-047. SUBSTITUTED FASTENERS IN CROSSBEAM IAW REO 670-53-11-265.
Part: UNKNOWN — ODOR (CABIN) · airframe 16,421 hrs · 11,407 cycles
ON CLIMBOUT FROM MIA THE SMELL OF SMOKE IN THE CABIN WAS REPORTED. EMERGENCY DECLARED, A/C RETURNED TO MIA LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 21-51-01-1A.
2009
Part: PROXIMITY SENSOR — DIRTY (NLG) · airframe 10,842 hrs · 7,577 cycles
ON CLIMBOUT FROM JFK RECEIVED NOSE GEAR DOOR WARNING MSG. FOLLOWED QRH, EMERGENCY DECLARED. A/C RETURNED TO JFK LANDED SAFELY. CLEANED AND INSPECTED PROX SENSORS AND TARGET PLATES. PERFORMED OPS CHECK OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM. NO DEFECTS NOTED.
2008
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 8,995 hrs · 6,273 cycles
FLIGHT 5289 - CO-PILOT'S WINDSHIELD CRACKED AT FL 390. DECLARED EMERGENCY, REDUCED ALTITUDE, DIVERTED TO ATL, LANDED WITHOUT INCIDENT. REPLACED WINDSHIELD. NO FURTHER DEFECTS.
2007
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 7,565 hrs · 5,338 cycles
FLIGHT 5347 - RIGHT SIDE SEAT TRACK RAILS HAVE CORROSION AND GOUGES BETWEEN FS 533 TO FS 830. BLENDED CORROSION/GOUGES AND REPLACED TRACK SECTION AT FS 784 - FS 830 IAW REO 670-53-00-074.
Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 7,565 hrs · 5,338 cycles
FS 280 CROSSBEAM AND RIGHT WEB ARE CORRODED BEYOND LIMITS. REPLACED FS 280 CROSSBEAM IAW REO 670-53-11-045 AND INSTALLED FABRICATED WEB IAW COMAIR EA 70-5311-01892.
Part: WARNING SYSTEM — MALFUNCTIONED (BLEED AIR SYS) · airframe 7,213 hrs · 5,080 cycles
FLIGHT 5535 - RECEIVED LEFT BLEED DUCT WARNING IN FLIGHT. EXTINGUISHED AFTER 50 SECONDS. RECEIVED LEFT BLEED MESSAGE, BLEED DUCTS CLOSED RESULTING IN PRESSURIZATION LOSS. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. PERFORMED TEST OF BLEED LEAK DETECTION SYSTEM AND INSPECTED DUCTS FOR LEAKS. NO DEFECTS FOUND.
Part: SLAT SYSTEM — MALFUNCTIONED · airframe 5,932 hrs · 4,203 cycles
FLIGHT 4994 - DURING CVG APPROACH RECEIVED A SLAT FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. PERFORMED FIM PROCEDURE 27-81-09-810-A01, NO MESSAGES PRESENT. SLAT OPERATION SATISFACTORY.
2006
Part: BPSU — FAULTY (SLATS) · airframe 5,451 hrs · 3,881 cycles
FLIGHT 5218 - SLAT FAIL CAUTION MESSAGE ON APPROACH, QRH COMPLETED. REMOVED AND REPLACED RIGHT SLAT BPSU.
Part: CONTROL UNIT — MALFUNCTIONED (SLAT/FLAPS) · airframe 5,336 hrs · 3,798 cycles
FLIGHT 5291- DURING ATL APPROACH RECEIVED A SLAT FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. PERFORMED RESET OF THE SLAT FLAP ELECTRONIC UNIT.
Part: ANTI-ICE VALVE — FAULTY (LT ENGINE) · airframe 3,705 hrs · 2,761 cycles
FLIGHT 5275 - EN ROUTE LGA-BTR, RECEIVED A LEFT ENGINE ANTI-ICE CAUTION MESSAGE, FLIGHT DIVERTED TO LGA. REPLACED THE LEFT ENGINE COWL ANTI-ICE VALVE.
Part: WARNING SYSTEM — FALSE ACTIVATION (LOW FUEL) · airframe 3,413 hrs · 2,579 cycles
FLIGHT 5276 - RT ENGINE LOW FUEL PRESSURE CAUTION. RESET SYSTEM, OPERATIONAL CHECK SATISFACTORY.
2005
Part: ACM — FAILED (LT AND RT) · airframe 2,835 hrs · 2,199 cycles
FLIGHT 4961- FOUND LT AND RT A/C PACK FAULT. CYCLED AIRCRAFT POWER. OPERATIONAL CHECK NORMAL.