N153PQ
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
UPON REMOVAL OF THE RT WING SIDE AILERON BUSHINGS, IT WAS FOUND THAT THE LUG LABELED -F- (HINGE NR 3 OTBD) HAS DAMAGE IN THE BORE & CURRENTLY MEASURES (0.8755""). REPAIRED LUG BORE OF THE R/H AILERON HINGE FITTING #3 AT WING TRAILING EDGE W.S.323.058 IAW HNIRJ REO 690-57-51-540 REV -- DATED 2026-06-11."
LEFT AFT OVERWING EMERGENCY DOOR HAS SUSPECTED CRACKED AT BASE OF STRIKER. COMPLIED WITH GREO 670-52-21-103 REV-.
RIGHT AFT OVERWING EMER. DOOR HAS SUSPECTED CRACK AT BASE OF STRIKER. COMPLIED WITH MHIRJ GREO 670-52-21-103 REV-- DATED 2024-11-06
R/H FWD OVERWING EMER. DOOR HAS SUSPECTED CRACK AT BASE OF STRIKER. COMPLIED WITH MHIRJ GREO 670-52-21-103 REV-- DATED 2024-11-06
THERE IS A POSSIBLE CRACK IN THE RIGHT-HAND VERTICAL STABILIZER DRAG ANGLE. STRIPPED PAINT FROM FWD DRAG ANGLE IAW CRJ900 SRM 51-26-01-001-001-A01. FOUND FWD DRAG ANGLE TO BE VISUALLY CRACKED 2.35"L, REMOVED FASTENERS FOR ACCESS FOR REPAIR IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01. CUT AWAY DAMAGE AND REMOVED ALL BURRS AND SHARP EDGES ON RT FWD DRAG ANGLE IAW SRM 55-31-00-201-001-A01, STEPS 5B(1), AND 5B(2). PERFORMED HFEC OF RT VSTAB DRAG ANGLE CUTLINE & UNDERLYING STRUCTURE IAW SRM 55-31-00-201-001-A01 STEP 5B(3). NO INDICATIONS NOTED AT THIS TIME. COMPLIED WITH STEPS 5B(4), 5B(7) & 5B(8) OF SRM 55-31-00-201-001-A01. COMPLIED WITH STEPS 5B (5,6, AND 11) OF SRM 55-31-00-201-001-A01. COMPLIED
UPON REMOVAL OF THE LT WING SIDE AILERON BUSHINGS, IT WAS FOUND THAT THE LUG -C- (HINGE NR 2 INBD) WAS PREVIOUSLY O/S & CURRENTLY MEASURES (0.8965"). COMPLIED WITH STEPS NR 1 & 2 OF IAW REO 690-57-51-541, REV -. ENSURED NO PREVIOUS BLENDING ON WING SIDE AILERON LUG -C-. ENSURED WING SIDE AILERON LUG -C- HAS A FINAL INTERNAL DIAMETER THAT MEASURES (0.8965"). C/W ET ON WING SIDE AILERON OVERSIZED BORE -C- IAW REO 690-57-51-541, REV -. NO INDICATIONS NOTED. COMPLIED WITH STEPS 4 & 6(A) OF REO 690-57-51-541 REV-. ALODINED THE BORE (A044). FABRICATED ONE O/S AILERON BUSHING, LPI PERFORMED IAW STEP 6(B) OF REO 690-57-51-541 REV. -. NO INDICATIONS NOTED APPLIED CAD PLATE TO FABRICATED BUSHING IAW REO 690-57-51-541 REV-. COMPLIED WITH STEPS 5, 7, 8 & 9 OF REO 690-57-51-541 REV -. INSTALLED O/S AILERON BUSHING USING NITROGEN. REAMED BUSHING. IAW REO 690-57-51-541.
FOUND 4 RT AILERON SIDE BUSHING LUGS -B-, -C-, -F- AND -G- TO BE PREVIOUSLY OVERSIZED. REPAIRED THE RT AILERON BUSHING LUGS BY REAMING TO 3RD OVERSIZE ON LUGS -B- & -G- AND 2ND OVERSIZE ON LUGS -C- & -F- IAW STEPS F.(1)-F.(4) OF GREO 670-57-61-237 REV--. PERFORMED LPI OF RT AILERON LUG BORES B, C, F, & G IAW REO 670-57-61-237 REV --, NO INDICATIONS NOTED. COMPLIED WITH STEPS F(7) & F(8) OF REO 670-57-61-237 REV --. FABRICATED 2 O/S AILERON BUSHINGS. FABRICATED 2 O/S AILERON BUSHINGS. PERFORMED LPI ON 4 NEWLY FABRICATED BUSHINGS FOR RT AILERON SIDE BUSHING LUGS LABELED -B-, -C-, -F-, AND -G- IAW REO 670-57-61-237 REV --, NO INDICATIONS NOTED. APPLIED CAD PLATE TO 4 FABRICATED BUSHINGS IAW STEP F(7) & F(8) OF REO 670-57-61-237 REV--. COMPLIED WITH REMAINING STEPS F.6, F.10-F.13 AND G IAW REO 670-57-61-237 REV --.
FOUND 2 EA LT AILERON SIDE BUSHING LUGS -C- AND -F- TO BE PREVIOUSLY OVERSIZED. REPAIRED 2EA LT AILERON SIDE BUSHING LUGS -C- & -F-, BY REAMING TO 1ST OVERSIZE IAW STEPS F.(1)-F.(4) OF GREO 670-57-61-237 REV--. PERFORMED LPI OF LT AILERON LUG BORES C AND F IAW REO 670-57-61-237 REV --, STEP F5. NO INDICATIONS NOTED COMPLIED WITH STEPS F(7) OF REO 670-57-61-237 REV -, STEP F(7), FABRICATED (QTY. 2) O/S AILERON BUSHINGS. PERFORMED LPI ON 2EA NEWLY FABRICATED BUSHINGS OF LT AILERON SIDE BUSHING LUGS -C- & -F- IAW REO 670-57-61-237, REV -, STEP F(9). NO INDICATIONS NOTED.CAD PLATED 2EA FABRICATED BUSHINGS PER STEP F(7) OF REO 670-57-61-237 REV-. COMPLIED WITH REMAINING STEPS F.6, F.10-F.13 AND G IAW REO 670-57-61-237 REV -. STEP F.8 .
EMERGENCY LIGHT EXTERNAL BY PAX DOOR INOP R/R EXTERNAL EMER LIGHT BY PAX DOOR IAW CRJ 900 AMM 33-51-15 OPS CHECK GOOD P/N ON/OFF: 8GH002473-08
"RH SERVICE DOOR EXTERNAL EMERGENCY LIGHT DS52 DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE SWITCHED ON. " "TROUBLESHOT SYSTEM AND DISCOVERED BULB WAS BURNT OUT FOR LIGHT DS52 & INSTALLED NEW SERVICEABLE BULB P/N 8GH002473-08 IAW CRJ 900 SRM 51-41-02-001-001-A01. ALSO DISCOVERED NO 2 BATTERY AT 5.2 VOLTS AND ALL THREE FUSES OHMED GOOD. SUSPECT BATTERY CHARGER TO BE BAD. REMOVED NO.2 ESPU BATTERY CHARGER P/N 11-0049 S/N 22488 IAW CRJ900 AMM 33-51-17-000-802-A02 & INSTALLED SERVICEABLE NO.2 ESPU BATTERY CHARGER P/N 11-0049 S/N 22736 IAW CRJ900 AMM 33-51-17-400-802-A02. OPS TEST GOOD IAW CRJ900 AMM 33-51-00-710-802-A03. "
PAX DOOR AFT WEB HAS MULTIPLE SPOTS OF CORROSION. INSTALLED NEW SERVICEABLE AFT WEB ASSY IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
PAX DOOR AFT WEB DRAG ANGLE IS CRACKED. INSTALLED NEW SERVICEABLE DRAG ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01
PAX DOOR AFT FORMER HAS MULTIPLE SPOTS OF CORROSION INSTALLED NEW PAX DOOR AFT FORMER, IAW CRJ900 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01
FLAP PANEL 684 GB IS CHAFED ON LEADING EDGE. REMOVED AND REPLACED PANEL 684GB
STRINGER 23R HAS CORROSION AROUND FASTENERS BTWEEN FS280 AND FS295 RECEIVED NEW STRINGER PN#SH670-31211-4U LOCATED AND DRILLED NEW STRINGER IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE STRINGER 23R BETWEEN FS 280 TO 333 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
F.S.319.70 FRAME TO FLOOR SILL FITTING IS CORRODED AT STGR 17R. REMOVED CORROSION ON FS319.70 FRAME TO FLOOR SILL FITTING AT STGR 17R IAW CRJ900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW CRJ-900 SRM 53-21-23-101-002-A02. REMOVED FITTING AT FS319.70 STR 17R IAW CRJ-900 SRM 51-42-21-001-001-A01. LOCATED AND DRILLED REPLACEMENT FITTING PN# SH670-31990-1 IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED NEW FITTING AT FS319.70 STR 17R IAW CRJ900 SRM 51-42-21-001-001-A01
PAX DOOR AFT DD7 INTERCOSTAL FOUND TO BE BENT AND BULGED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR INTERCOSTAL DD7 AT AFT SIDE IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 PN: 601R318825-1
PAX DOOR ANGLE C AT DD7A FOUND TO BE CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE ANGLE C AT DD7A IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01
FS 280 FLOORBEAM L/H IS CORRODED, REPLACE REQUIRED. REMOVED AND REPLACED IAW CRJ 900SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-12-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01
LOWER FRAME SECTOR , FS 364.00, STRGR.26L - 26R CORRODED REMOVED AND REPLACED, LOWER FS 364.00 FRAME SECTOR,IAW CRJ 900 SRM'S,#53-21-23-201-008-A01,#51-40-11-001-001-A01, #51-42-06-001-001-A01, #51-42-21-001-001-A01, AND MHIRJ EO'S, #SH670-32090(SNEIO-01) & #SH670-32050(SNEIO-16),BOTH REV --, & DATED 26-10-20.
STRINGER 25L FROM F.S.295 TO F.S.319.70 IS CORRODED. REMOVED AND REPLACED IAW CRJ 900SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.
RIGHT SIDE SEAT RAIL BETWEEN FS 785.00 AND 847+16 IS CORRODED REPLACED RH SIDE SEAT RAIL P/N SH670-36260-5 FROM FS 785.00 TO 847+16 IAW CRJ 900 AMM 53-00-49-400-801(A07).
RBL9 FLOOR SEAT TRACK FROM F.S.485 TO F.S.581 IS CORRODED. INSTALLED NEW SEAT TRACK PN SH690-33407-1 IAW CRJ 900 AMM 53-00-49-400-801-A07.
RBL9 FLOOR SEAT TRACK FROM F.S.581 TO F.S.661+32 IS CORRODED. INSTALLED NEW SEAT TRACK PN SH690-33404-1 IAW CRJ 900 AMM 53-00-49-400-801-A07.
R/H SIDE SEAT RAIL IS CORRODED FROM F.S.661+16 TO 677. REMOVED AND REPLACED R/H SIDE SEAT RAIL FROM F.S. 661+16 TO F.S. 677 P/N SH690-36283-1 IAW CRJ-900 AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07
LEFT SIDE SEAT RAIL BETWEEN FS 744.00 AND 752.00 IS CORRODED INSTALLED NEW SEAT RAIL IAW CRJ 900 AMM 53-00-49-400-801-A07
280 CROSSBEAM FWD "J" ANGLE IS CORRODED. REMOVED AND REPLACED FWD âJâ ANGLE AT FS280 BETWEEN LBL12 TO RBL12 IAW CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
LEFT SIDE SEAT RAIL BETWEEN FS 785.00 AND 847+16 IS CORRODED, REMOVED SEAT RAIL IAW CRJ 900 AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT RAIL PART NUMBER SH670-36260-5 IAW CRJ 900 AMM 53-00-49-400-801-A07
FS280 FLOORBEAM R/H IS CORRODED. REMOVED AND REPLACED RH FS 280 FLOORBEAM IAW CRJ 900 SRM 51-42-06-001-001-A01 51-42-21-001-001-A01, 51-42-12-001-001-A01, 51-42-22-001-001-A01
L/H SIDE SEAT RAIL IS CORRODED FROM F.S.661+16 TO 677. INSTALLED NEW SEAT RAIL IAW CRJ 900 AMM 53-00-49-400-801-A07.
LBL9 FLOOR SEAT TRACK FROM F.S.661+32 TO F.S.693 IS CORRODED. INSTALLED NEW SEAT TRACK IAW CRJ 900 AMM 53-00-49-400-801-A07.
RBL9 FLOOR SEAT TRACK FROM F.S.661+32 TO F.S.693 IS CORRODED. INSTALLED NEW SEAT TRACK IAW CRJ 900 AMM 53-00-49-400-801-A07.
LBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 693 TO F.S. 830. FABRICATED, LOCATED AND DRILLED AND INSTALLED NEW SEAT TRACK ON LBL 9 BTWN FS 693 TO FS 830 IAW CRJ900 SRM 51-40-11-001-001-A01, 53-00-49-201-002-A01 AND CRJ 900AMM 53-00-49-400-801-A07.
LBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 985 TO F.S. 1000. FABRICATED SEAT TRACK RBL 9 FS 849-985 FROM 20276-288-0-0A IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 53-00-49-201002-A01. INSTALLED IAW CRJ 900 AMM 53-00-49-400-801-A07.
LBL9 FLOOR SEAT TRACK FROM F.S.581 TO F.S.661+32 IS CORRODED INSTALLED NEW SEAT TRACK IAW CRJ 900 AMM 53-00-49-400-801-A07.
RIGHT SIDE SEAT RAIL BETWEEN FS 744.00 AND 752.00 IS CORRODED, REMOVED AND REPLACED RH SIDE SEAT RAIL (PN: SH690-36285-1) BETWEEN FS 744 AND FS 752 IAW CRJ-900 AMM 53-00-49-000-801 (A07) AND CRJ-900 AMM 53-00-49-400-801 (A07)
LEFT SIDE SEAT RAIL BETWEEN FS 913.00 AND 969.00 IS CORRODED, REMOVED AND INSTALLED NEW LH SEAT RAIL PN SH690-37542-1 BETWEEN FS913.00 AND FS969.00 IAW CRJ900 AMM 53-00-49-400-801 (CONFIG A07).
FOUND HINGE #2 AILERON WING FITTING NOMINAL OUTBOARD LUG TO BE DAMAGED. REPAIRED LEFT AILERON #2 WING HINGE FITTING IAW MHIRJ REO 690-57-51-276
FWD CARGO DOOR LOWER SEAL RETAINER IS DAMAGED IN MULTIPLE LOCATIONS. FOUND FWD CARGO DOOR LOWER SILL RETAINER TO BE OUT OF LIMITS IAW CRJ 900 SRM 51-42-06-001-001-A01. REMOVED LOWER SEAL RETAINER FROM FWD CARGO DOOR IAW CRJ900 SRM 51-42-06-001-001-A01. INSTALLED LOWER SEAL RETAINER FROM FWD CARGO DOOR IAW CRJ900 SRM 51-42-06-001-001-A01.
RBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 830 TO F.S. 849. REMOVED AND REPLACED CORRODED RBL9 SEAT TRACK FROM FS830 TO FS849 WITH NEW SERVICEABLE SEAT TRACK PN BA690-30000-6959 IAW CRJ900 AMM 53-00-49-400-801-A01
RBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 849 TO F.S 985. FABRICATED SEAT TRACK RBL 9 FS 849-985 FROM 20276-288-0-0A IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 53-00-49-201002-A01. INSTALLED IAW CRJ 900 AMM 53-00-49-400-801-A07.
LBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 830 TO F.S. 849 INSTALLED NEW SEAT TRACK PN BA690-30000-6959 IAW CRJ 900 AMM 53-00-49-400-801-A07
STGR 26L IS CORRODED BETWEEN F.S. 1000 TO F.S. 1031 INSTALLED NEW SERVICEABLE STRINGER 26L AND CLEATS FROM FS 977 TO FS 1098 IAW CRJ900 SRM 53-00-03-201-001-A02
VERTICAL STAB L/H AFT DRAG ANGLE IS CRACKED INSTALLED NEW AFT DRAG ANGLE ON LH VERTICAL STAB IAW CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-10-001-001-A01.
JACK PAD INTERCOSTAL ON RH SIDE BETWEEN FS 265 TO 280 IS CORRODED ON ATTACH FLANGE. LOCATED AND DRILLED LH AND RH JACK PAD INTERCOSTALS IAW CRJ900 SRM 51-40-11-001-001-A01
STRINGER 24L BETWEEN FS 485.00 AND 501.00 IS CORRODED. INSTALLED STRINGER 24L BETWEEN FS 477.40 TO FS 501.00+3 IAW MHIRJ AVIATION REO # 690-53-31-667 REV.P2 DATE 2022-10-06
F.S.1000 TO F.S.1031 STRINGER 25L IS CORRODED REPAIRED STRINGER 25L BETWEEN F.S.1015 TO F.S.1047 IAW MHIRJ REO 690-53-61-1115
F.S. 1015 FRAME IS CORRODED BETWEEN STGR 27 TO STGR 26L NSTALLED NEW SECTION FRAME AT FS 1015 BETWEEN STGR 25R TO STGR 19L IAW CRJ-900 SRM 53-00-06-201-001-A03
PAX DOOR FWD INTERCOSTAL DD3 FOUND TO BE CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR FWD INTERCOSTAL DD3 IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
PAX DOOR FWD FORMER FOUND TO BE CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR FWD FORMER IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 PN:601R318031-5
H SPLICE AT F.S.629 STRINGER 26L IS CORRODED REPAIRED JOINT SPLICE (H SPLICE) AT F.S.629 IAW MHIRJ REO 690-53-31-670
BL 9 FLOOR BEAM IS CORRODED BETWEEN F.S. 1015 TO F.S. 1069 FLOOR BEAM AT LBL 9 BETWEEN F.S. 1015 TO F.S. 1069 REPLACED IAW CRJ-900 SRM 53-00-41-201-001-A03.
LBL9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 849 TO F.S. 985 INSTALLED A NEW SEAT TRACK P/N 20276-288-0-0A IAW CRJ900AMM 53-00-49-000-801(A07)
INTERCOSTAL 20R FROM F.S.319.70 TO F.S349 IS CORRODED LOCATED AND DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL FOR STR 20R IAW CRJ900 SRM 51-40-11-001-001-A01 P/N SH670-32004-1
PASSENGER DOOR SURROUND STRUCTURE LOWER SILL ANGLE IS CORRODED
PAX DOOR INNER SKIN HAS MULTIPLE SPOTS OF CORROSION INSTALLED NEW PAX DOOR INNER SKIN, IAW CRJ900 SRM 51-40-06-001-001-A01, 51-40-11-001-001-A01
STRINGER 23L IS CORRODED BETWEEN F.S.1000 TO F.S.1031 REPAIRED STRINGER 23L IAW MHIRJ REO 690-53-61-1127
STRINGER 22R IS CORRODED AROUND FASTENER BETWEEN F.S.280 AND F.S.295 REMOVED AND REPLACED STRINGER 22R
STGR 21L IS CORRODED BETWEEN F.S. 1015 TO F.S. 1031. INSTALLED NEW REPLACEMENT STRINGER, SPLICES, AND SHIM IAW CRJ900 SRM 53-00-03-201-001-A02
STGR 22L IS CORRODED BETWEEN F.S. 985 TO F.S. 1000 CUT STRINGER 22 L AT FS 1007 AND REMOVED STRINGER SEGMENTS IAW CRJ 900 SRM TASK 53-00-03-201-001-A02. INSTALLED NEW SERVICEABLE STRINGER AND SPLICE REPAIR AT STGR 22L BETWEEN FS. 985 TO FS. 1098 IAW CRJ-900 SRM 53-00-03-201-001-A02
INTERCOSTALS AT STGR 19R FWD AND AFT OF FRAME F.S.661+90 ARE CORRODED. FABRICATED AND INSTALLED NEW SERVICEABLE AFT INTERCOSTAL ON STGR 19R AT F.S.661+90 IAW CRJ-900 SRM 51-24-16-001-001-A01. USED DRAWING # SH690-39112
FRAME AT F.S.613 IS CORRODED BETWEEN STRINGER 24L AND 26R.
STRINGER 19R BETWEEN F.S.661+16 TO F.S.661+32 IS CORRODED FABRICATED, AND INSTALLED REPLACEMENT STRINGER 19R BETWEEN FS 597 AND FS 661+90 AND STRINGER SPLICES 3EA BTW FS 597-FS 613, FS 645-FS 661, FS 661+74-FS 661+90 IAW CRJ900 SRM 53-00-03-201-001-A01
STRINGER 27 BETWEEN F.S.250 TO F.S.265 IS CORRODED REMOVED AND REPLACED STRINGER 27
STGR 24L IS CORRODED BETWEEN F.S. 1000 AND F.S. 1015 REMOVED AND REPLACED STGR 24L BETWEEN F.S. 1000 AND F.S. 1015
STRINGER 21R HAS CORROSION AROUND FASTENERS BETWEEN FS280 AND FS 295. REMOVED AND REPLACED WITH NEW STRINGER PN#SH670-31636-1U LOCATED AND DRILLED NEW STRINGER IAW CRJ900 SRM 51-40-11-001-001-A01.
STRINGER 19R IS CORRODED AROUND FASTENERS BETWEEN FS 280-333. REMOVED AND REPLACED STRINGER 19R BETWEEN FR280 - FR333 IAW CRJ900 SRM 51-42-06-001-001-A01
FUSELAGE FRAME F.S.533 IS CORRODED BETWEEN STRINGER 17L AND 18L REPAIRED FRAME F.S.533 IAW CRJ 900 SRM 53-00-06-201-001-A03
PAX DOOR INTERCOSTAL DD7A HAS MULTIPLE SPOTS OF CORROSION LOCATED DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL DD7A IAW CRJ900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
PAX DOOR INTERCOSTAL DD4 HAS MULTIPLE SPOTS OF CORROSION LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR INTERCOSTAL DD4 MID IAW CRJ900 SRM 51-40-11-001-001-A01 51-42-21-001-001-A01 AND 51-42-06-001-001-A01
PAX DOOR INTERCOSTAL DD3 HAS MULTIPLE SPOTS OF CORROSION LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR INTERCOSTAL DD3 MID IAW CRJ900 SRM 51-40-11-001-001-A01 51-42-21-001-001-A01 AND 51-42-06-001-001-A01
PAX DOOR INTERCOSTAL DD2 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED WITH NEW SERVICEABLE DD2 INTERCOSTAL IAW CRJ900 SRM 51-40-11-001-001-A01 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
FS 250 RBL9 AND LBL9 FRAME IS CORRODED INSTALLED NEW FRAME AT F.S. 250 BETWEEN 26L AND 26R IAW MHIRJ REO # 690-53-11-1470
RBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 693 TO F.S. 830. INSTALLED NEW SEAT TRACK AT RBL 9 FS 693 TO 830, P/N 20276-228-0-0A IAW CRJ 900 AMM 53-00-49-400-801(A07).
PAX DOOR FWD AND AFT WEB HAS MULTIPLE SPOTS OF CORROSION INSTALLED NEW SERVICEABLE FWD AND AFT WEB ASSY IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
FUSELAGE FRAME F.S.549 IS CORRODED BETWEEN STRINGER 17L AND 18L. REPAIRED FRAME SECTOR F.S.549 IAW MHIRJ REO 690-53-31-679
STRINGER 19R IS CORRODED AT FS661+90 INSTALLED NEW SERVICEABLE STRINGER 19R PN:SH690-33151-5A FS661+74 TO 661+90 PER CRJ900 SRM 53-00-03-201-001-A02
PANEL 599BB HAS CHAFE, REQUIRES EVALUATION AND BLEND REMOVED AND REPLACED PANEL 599BB
AFT RIGHT OVERWING EMERGENCY LIGHT FOUND INOP DURING R/C. R&R AFT RIGHT OVERWING EMERGENCY HOUSING IAW CRJ 900 AMM 33-51-15 & CRJ 900 ESPM 20-16-00. OPS CHECK GOOD.
DAMAGE FOUND ON STRUCTURE ON AFT SIDE OF AFT CARGO DOOR SURROUND - AFT CARGO DOOR, DOOR ASSIST PULLEY GUIDE SUPPORT BEAM WAS REPAIRED PER EA CRJ953-12292. THIS IS A MAJOR REPAIR-- REF NRWC 804069 OF 912.1 WP 11/01/21 FOR REPA IR OF THE AFT CARGO DOOR BEAM FS 1047.00 PN MM670-35502-010, CL600-2D24 USING EA CRJ953-12292 FOR COMPLETION OF BEAM REPAIR. THIS ENTRY COMPLIES WITH GMM 3-03 D 7 A) AND B)
SERVICE DOOR EMERGENCY LIGHT AND FWD CABIN CEILING EMERGENCY LIGHTS WON'T ILLUMINATE. REPLACED EMERGENCY LIGHT BATTERY PACK PS36 PER JOB CARD 33-900-701. OPS CHECK GOOD. P/N OFF AD-2013-1A, S/N OFF 103201, P/N ON 2013-1ASMI, S/N ON 11173.
CRACKED LONGITUDINAL FLOOR BEAM LBL 12 AND FS 280. BELOW COCKPIT. FLOORBEAM LBL 12 AND FS 280 BELOW COCKPIT WAS REPAIRED PER REO 690-53-11-1159 REV. -- AND REO 690-53-11-431 REV. -A
CRACKED PASSENGER DOOR LINTEL AT STGR 3L BETWEEN FS 280 / FS 295. THE LINTEL WAS REPAIRED IAW ENGINEERING ORDER R53568 AND REO 670-53-21-493 REV. D
WEAR IN ACCESS PANEL NBR 584JB,584LB,599BB AND 699AB. ACCESS PANEL NBR 584LB WAS REPAIRED PER EA CRJ957-09427 REV: IR, ACCESS PANEL NBR 584JB WAS REPAIRED PER EA CRJ957-09418 REV: IR, ACCESS PANEL NBR 599BB WAS REPAIRED PER EA CRJ957-09422 REV: IR AND ACCESS PANEL 699AB P/N: 601R13440-2 WAS VERIFIED PER A.I.P.C. 57-60-32 FIG. 1A ITEM -15 AND NEW ACCESS IS INSTALLED UNDER OPENING AND CLOSING JOBCARD: FORM MM48 REV. 2/2015.
DURING NDT INSPECTION, CRACK OF 0.500 INCH WAS FOUND ON MAIN AVIONICS COMPARTMENT DOOR HANDLE HOUSING. NEW DOOR HANDLE HOUSING WAS REPLACED PER CRJ-900 S.R.M. 51-42-21-001-001-A01
CORROSION ON INTERCOSTAL RBL 2 BTW FS 349 TO 364 AT E/E COMPARTMENT. INTERCOSTAL RBL 2 BTW FS 349 TO 364 AT E/E WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01 "
CRACKED FLOORBEAM RBL 12 AND FS 280. BELOW COCKPIT. FLOORBEAM RBL 12 AND FS 280. BELOW COCKPIT WAS REPAIRED PER CRJ-900 REO 690-53-11-1159 REV--
CORROSION ON INTERCOSTAL LBL 2 BTW FS 349 TO 364 AT E/E COMPARTMENT. THE INTERCOSTAL WAS REPLACED SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01. "
AFTER BUSHINGS REMOVAL CORROSION ON HOUSING OF FITTINGS WAS FOUND AT NLG WHELL WELL (FYT). FITTINGS AT NLG WHELL WELL WERE REPLACED PER CRJ-900 SRM 51-42-21.
CORROSION ON SKIN DRAINAGE FS 280 TO 295 BTW STGR 26R-26L AT E/E COMPARTMENT. SKIN DRAINAGE WAS REPLACED PER CARD R53579 STEP37 (A)(B) FIGURE 8.
CRACK ON FLOOR PANEL SUPPORT AT LBL 12 AND FS 265 - 280. FLOOR PANEL SUPPORT AT LBL 12 AND FS 265 - 280 WAS REPLACED PER SRM 51-42-06-001-001-A01
CORROSION ON FRAME BS 349 BTW STGR 26RH-27RH ING THE E/E COMPARTMENT. THE FRAME WAS REPAIRED IAW EA:CRJ953-09447 REV. IR
CORROSION ON STRINGER 26L FROM BS 280 TO 364. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
CORROSION ON STGR 27 AT E/E COMPARTMENT BTW FS 280 - 349. CORROSION ON STGR 27 AT E/E COMPARTMENT BTW FS=280/349 WERE REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
CORROSION ON FLOOR SUPPORT LBL 5 BTW FS 349 TO 364 IN THE E/E COMPARTMENT. FLOOR SUPPORT REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.
CORROSION ON STRINGER 26R FROM BS 280 TO BS 364 AT MAIN AVIONICS COMPARTMENT. STRINGER 26R WAS REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. SH670-31372-4
CRACKED STOPPERS (2 E/A) OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT. STOPPERS WERE REPLACED PER AMM 53-62-34-000-801 CONF. A01 AND AMM 53-62-34-400-801 CONF. A01. "
CORROSION ON ANGLE MOUNTING OF GALLEY SERVICE DOOR SURROUND STRUCTURE. ANGLE MOUNT WAS REPLACED PER SRM 51-42-06-001-001-A01. "
CORROSION ON INTERNAL STGR 19R BTW FS364 TO FS379. THE STRINGER WAS REPLACED PER SRM 51-42-06-001-001-A01.
"LATE FINDING: CORROSION ON ANGLE STGR 21R BTW FS364 TO FS379. AMAGE ANGLE ON STGR 21RH BTW FS 364 TO FS 379 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 PAR.6. STGR 21RH WAS MEASURED AS FOLLOW: ORIGINAL THICKNESS 0.080¨, REMAINING THICKNESS 0.038¨ IT WAS FOUND OUT OF LIMITS PER CRJ/900 SRM 53-00-00-101-001-A01.
CORROSION ON PROTECTOR PLATE SUPPORTS AND ANGLES OF GALLEY SERVICE DOOR SURROUND STRUCTURE. SUPPORTS AND ANGLES OF GALLEY SERVICE DOOR SURROUND STRUCTURE, WERE REPLACED IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.
"INITIAL INSPECTION: CORROSION ON INTERNAL PRODUCTION DOUBLER IN BS 295 TO 310 BETWEEN STGR 26LH TO 26RH IN THE E/E COMPARTMENT. INTERNAL PRODUCTION DOUBLER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND 51-42-20-001-001-A01.
"LATE FINDING: CORROSION ON INTERNAL STGR 22R BTW FS333 TO FS349. CORROSION LEVEL 2 ON INTERNAL STGR 22R BTW FS333 TO FS349 AT MAIN AVIONICS COMPARTMENT E/E WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
CORROSION ON STGR SPLICE 26L, BS 333 AT MAIN AVIONICS COMPARTMENT. REMOVED THE STRINGER SPLICE 26L, A NEW SPLICE WAS INSTALLED IAW SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.
CORROSION ON STRINGER SPLICE 21R AND BS 333. THE STRINGER SPLICE WAS REPLACED IAW SRM 51-42-06-001-001-A01. "
CORROSION ON INTERCOSTAL E/E COMPARTMENT BTW FS=310/319 AND STGR 20R .INTERCOSTAL E/E COMPARTMENT BTW FS=310/319 AND STGR 20R WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01-AND SRM 51-42-21-001-001-A01.
CORROSION ON INTERNAL FUSELAGE STRUCTURE AT SETTLEMENT AREA OF HYDRAULIC LOWER ACCESS PANEL 195AB. SUPPORT ON SETTLEMENT AREA OF HYDRAULIC LOWER ACCESS PANEL (195AB) WAS REPLACED IAW SRM 51-42-10-001-001-A01 AND INTERNAL FUSELAGE STRUCTURE AT SETTLEMENT AREA OF HYDRAULIC LOWER ACCESS PANEL WAS BLENDED OUT AND WAS FOUND WITHIN LIMITS.
CORROSION ON INTERNAL STGR 21R BTW FS394 TO FS409. STRINGER 21R WAS REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
"INITIAL INSPECTION: CORROSION ON INTERNAL STGR 18R BTW FS394 TO FS409. THE STRINGER WAS REPAIRED IAW SRM 53-00-03-201-001-A02, FIG.53-00-03-995-807,SOLUTION II.
CORROSION ON INTERNAL STRINGER 21R BETWEEN BS 364 - 379. THE STRINGER WAS REPLACED IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. "
"LATE FINDING: CORROSION ON SPLICE 22R BTW FS333 TO FS349 (E/E). CORROSION ON SPLICE 22R BTW FS333 TO FS349 AT MAIN AVIONICS COMPARTMENT, NEW SPLICE 22R BTW FS333 TO FS349 AT MAIN AVIONICS COMPARTMENT (E/E) WAS INSTALLED PER CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
CORROSION ON STRINGER SPLICE 27, BS 333 IN THE MAIN AVIONICS COMPARTMENT. THE STRINGER SPLICE NBR 27 STA FS= 333 AT MAIN AVIONICS COMPARTMENT. (E/E) WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.
CORROSION ON INTERCOSTALS AT E/E COMPARTMENT BTW FS=310/349 AND STGR 21L. INTERCOSTALS AT E/E COMPARTMENT BTW FS=310/349 AND STGR 21 LH (2 E/AS) WERE REPLACED PER CRJ/900 SRM 51-42-21-001-001-A01.
CORROSION ON STGR 20R AT E/E COMPARTMENT BTW FS=280/295. STRINGER 20 RH BTW FS=280 AND FS=315 WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01. "
CRACK IN CANISTER WELDED NO. 3 ASSY LEFT OUTER WINGBOX FUEL TANK (SM). CANISTER WELDED THE NR 3 ASSY LEFT OUTER WINGBOX FUEL TANK WAS REPAIRED AND ATTENDED PER REO 670-57-42-577 REV.--
INITIAL INSPECTION:CORROSION ON STGR SPLICE NBR 26 RH STA FS= 333 AT MAIN AVIONICS COMPARTMENT. STGR SPLICE 26 RH STA FS= 333 AT MAIN AVIONICS COMPARTMENT WAS MEASURED AS FOLLOW: ORIGINAL THICKNESS 0.063¨, REMAINING THICKNESS 0.055¨ IT´S OUT OF LIMITS, REPLACED PER SRM 53-00-00-101-001-A01, 51-42-06-001-001-A01
CRACK IN CANISTER WELDED NO. 3 ASSY RIGHT OUTER WINGBOX FUEL TANK. CRACKED CANISTER WELDED NR 3 ASSY RIGHT OUTER WINGBOX FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. -- .
CORROSION ON FLOOR STRUCTURE GALLEY FITTING SUPPORT BTW FS 280/295 AND RBL 17 IN REF EO R53520 STEP 7. THE FITTING WAS REPLACED IAW SRM 51-42-21-001-001-A01.
CRACK IN BRACKET SUPPORT OF CANISTER WELDED NO. 1 ASSY RIGHT OUTER WINGBOX FUEL TANK. NEW BRACKET SUPPORT OF CANISTER WELDED NR 1 ASSY RIGHT OUTER WINGBOX FUEL TANK WAS DRILLED PER SRM 51-40-11-001-001-A01 AND NEW BRACKET SUPPORT OF CANISTER WELDED NR 1 ASSY RIGHT OUTER WING BOX FUEL TANK WAS INSTALLED PER SRM 51-42-06-001-0.
CRACK ON BOX OF THE EXTERNAL POWER RECEPTACLE AT THE FWD FUSELAGE. EXTERNAL POWER BOX WAS FABRICATED PER EA NO: CRJ953-09257 REV.IR ,AND REPAIR PARTS, EXTERNAL POWER BOX WAS INSTALLED IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
BOTH (LEFT&RIGHT) AFT OVERWING EMERGENCY LIGHTS WILL NOT ILLUMINATE. R & R AFT EPSU BATTERY CHARGER ASSEMBLY P/N ON/OFF 11-0049 S/N ON 22480S/N OFF 22621 IAW CRJ900 AMM 35-51-17. R+R EPSU BATTERY PACK PS38 P/NON AD-2013-1A S/N ON 178193 P/N OFF 2013-1ASMI S/N OFF 11618 IAW JC 33-900-701. LH AND RH AFT OVERWING EMERGENCY LIGHTS OPS CHECK GOOD.
DURING OPERATIONAL CHECK OF EMERGENCY LIGHTS NOTED INTERMITTANT ILLUMINATION OF EXIT LIGHTS AT OVERWING EXITS. REMOVED & REPLACED EMERGENCY BATTERY PACK AT POSITION PS43, IAW AMM CH 33-51-17. OPS CHECK GOOD.
UPDATE ON PROBLEM DESCRIPTION. DURING EE-900 INSPECTION NOTED SEAT 1C MISSING LIFE VEST. INSTALLED LIFE VEST BOX STRAP ON PASS SEAT 1C IAW TS 005235B.
FIRST OFFICER`S OXYGEN MASK WAS BROKEN. R & R THE OXYGEN MASK.IAW AMM 35-11-12, OPS CHECKED GOOD IAW AMM 35-10-00. OK FOR SERVICE.
GEAR DISAGREE, NOSE WHEEL STAYED DOWN WHEN GEAR RETRACTED. INSPECTED THE NOSE STRUT. SERVICED THE NOSE STRUT WITH OIL AND NITROGEN IAW AMM 12-12-32, JACKED THE AIRCRAFT IAW 07-12-03, PERFORMED A GEAR RETRACTION AND EXTENTION, NO FAULTS NOTED. AIRCRAFT OKAY TO RETURN TO SERVICE IAW 900-12-710-700
LEFT WING AFT EMERGENCY LIGHT INOPERATIVE. RECONECTED CONNECTOR PLUG BEHIND SIDE WALL PANEL 16AB AND REMOVED & REPLACED LIGHT ASSY IAW AMM 33-51-15. AND REMOVED & REPLACED PCB5 RELAY K135 IAW AMM 24-06-01. OP CHECKED GOOD.
EMERGENCY LIGHT OVERWING RT SIDE INOPERATIVE. REMOVED & REPLACED RT SIDE OVERWING AFT LIGHT ASSY IAW AMM 33-51-15 OPS CHECKED GOOD.
RIGHT WING FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-51-15. OPS CHECKED GOOD.
EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-11. REMOVED AND REPLACED THE BATTERY CHARGER NR 1 IN AVIONICS COMPARTMENT IAW AMM 33-51-17.
EXIT SIGN IN THE GALLEY IS MISSING. REPLACED THE SIGN IAW AMM 33-51-05.
RT WING FWD EMERGENCY EXIT LIGHT INOPERATIVE. EXTERIOR EMERGENCY LIGHTS, FORWARD OVERWING EMERGENCY LIGHT ON EACH SIDE. TROUBLESHOOT RT WING FWD EMERGENCY EXIT LIGHT IAW FIM 33-51-00 AND WIRING DIAGRAM 33-51-01. FOUND WIRE AT P396 BROKEN REPAIR WIRE IAW ESPM 20-16-00. PERFORM OPS CHECK IAW AMM 33-50-00. OPS CHECK GOOD. EMERGENCY LIGHTS RETURN TO SERVICE.
BATTERY HOUSING WIRING DAMAGED. R & R MEGAPHONE IAW AMM 25-61-14. AIPC REF 25-61-14, FIG. 1K, ITEM 5.
RT REAR EXIT EMERGENCY LIGHT INOPERATIVE. R & R EXIT EMERGENCY LIGHT ASSY, RT FWD, IAW AMM 33-51-15. R & R ESPU BATTERY PACK NR 3 IAW AMM 33-51-17.
CENTER CARGO BAY DOOR SEAL RETAINER BENT AT FORWARD LOWER CORNER. PERFORMED PERMANENT REPAIR TO FORWARD LOWER CORNER OF CENTER CARGO BAY SEAL RETAINER IAW EC/TC REO 690-52-35-013. REPAIR CLASSIFIED AS MAJOR IAW GMM 5-3.
COMPLY WITH PERMANENT REPAIR OF H/S BELLCRANK SUPPORT FITTING INSTALLATION LT SIDE, RT SIDE ATTACHMENT FASTENERS IAW REO 69055-11-069. COMPLIED WITH PERMANENT REPAIR OF LT SIDE, RT SIDE BELLCRANK SUPPORT FITTINGS IAW EC/TC REO 690-55-11-094. COMPLIED WITH EC/TC 690-55-11-094. REMOVED FAIRING 326CT IAW AMM 55-32-56-000-809. REINSTALLED OF THE AFT FRAME AND FAIRINGS 326CT IAW AMM 55-32-86-400-809 A01, OPS CHECK GOOD.
INTERCOSTAL BETWEEN FS 349 TO FS 364 AT CORRODED. R & R INTERCOSTAL IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 DWG SH670-32075 AT STR 27R RT WING FS 349 & 364.
WHILE ADDRESSING CORROSION ON STR 25R DISCOVERED CORROSION AROUND FASTENERS ON STR SPLICE 26R BETWEEN FS 319-333. BLENDED CORROSION REF SRM 51-21-06-001001-A01 & SRM 51-42-06-001-001-A01. DAMAGE EXCEEDS ALLOWABLE LIMITS. R & R STRINGER SPLICE IAW SRM 51-42-01-001-001-A01.
DURING REMOVAL OF BS 280 FLOORBEAM ANGLE CORRODED AT LBL 9 FWD SIDE. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 690-53-11-859, STEPS 1-7, EM12174 3/10/16 (PB) M/A: 4.
LT SIDE SEAT TRACK AT FS 785.15 CORRODED. R & R COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV M.
FLOORBEAM ANGLE AT FWD SIDE OF BS 280 FLOORBEAM HAS CORROSION. REMOVED FLOORBEAM ANGLE AT FWD SIDE OF BS 280 IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-12-001-001-A01. LOCATED AND DRILLED NEW FLOORBEAM ANGLE IAW SRM 51-40-11-001-001-A01. LOCATED AND DRILLED FOUR HOLES AT RBL AND LDL9 AND INSTALLED RIVETS FLOOR HOLES IN TOP, INSTALLED 11 LOCK FASTENERS INBD LT SIDE AND 12 LOCK FASTENERS INBD RT SIDE IAW SRM 51-42-08-001-001-A01 AND 51-42-21-001-001-A01 FASTENER CALLEDOUT FROM DWG SB670BA-53-041. COMPLETED INSTALLION OF FS 280 FLOORBEAM ANGLE IAW SRM 51-42-06-001-01-A01 AND 51-42-21-001-001-A01 FASTENER REF DWG SB670BA-53-041.
PAX DOOR SILL ANGLE HAS CORROSION. REMOVED PAX DOOR SILL MID CAP ANGEL IAW SRM 51-41-00-001-001-A01. LOCATED, DRILLED AND INSTALLED NEW MID CAP ANGLE IAW SRM 51-42-06-001-001 A01. REMOVED PAX DOOR SILL LOWER ANGLE IAW 51-42-06-001-001 A01. LOCATED AND DRILLED NEW LOWER ANGLE IAW SRM 51-42-06-001-001 A01. INSTALLED SOLID RIVETS THROUGH ANGLE AND SILL PLATE IAW SRM 51-42-06-001-001 A01. INSTALLED NEW LOWER ANGLE IAW SRM 51-42-06-001-001 A01
FLOOR SILL FWD OF SERVICE DOOR IS CORRODED. FLOOR SILL FWD AT SERVICE DOOR CORROSION IS OUT LIMITS. REMOVED FWD OF SERVICE DOOR FLOOR SILL IAW SRM 51-42-06-001-001-A01. LOCATED FASTENER HOLES IN NEW SERVICABLE SILL ANGLE AD PARTIALLY INSTALLED SILL BETWEEN FS 280 AND FS 319 IAW SRM 51-40-11-001-001 A01, 51-42-06-001-001 A01, 51-42-15-001-001 A01 DWG SH690-32170. COMPLETED FASTENER INSTALLATION IN SILL ANGLE ASSY IAW SRM 51-42-06-001-001 A01, 51-42-21-001-001 A01, AND DWG SH690-32170.
ANGLE CORRODED AT RBL 9, FS 333.00. R & R IAW SRM 51-42-06-001-001-A01.
SEAT TRACK BS 785.15 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000/900-801-A07.
SEAT TRACK BS 752.50 CORRODED. R & R IAW AMM 53-00-49-000-801-A07 AND AMM 53-00-49-400-801-A01.
SEAT BS FS 720.85 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND AMM 53-00-49-400-801-A07.
LT SIDE SEAT TRACKS AT FS 752.50 CORRODED. R & R SEAT TRACK IAW SRM 51-41-00-001-001-A01.
SEAT TRACK AT BS 720.85 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
LEFT SIDE SEAT TRACK AT BS 597 - 661 AT STRINGER 15L. R & R LT SIDE SEAT TRACK AT FS 597.00 TO 661.00 IAW AMM 53-00-49-000-801A-07 AND 53-00-49-400-801-A07.
LT SIDE SEAT TRACK CORRODED AT FS 453 AT STR 15L. R & R THE SEAT TRACK AT IAW AMM 53-00-49-000-801A-07 AND 53-00-49-400-801-A07.
SEAT TRACK AT BS 349 & RBL 9 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-801A-07 AND 53-00-49-400-801-A07.
BETWEEN FS 913.00 AND FS 927.00 AT STR 27 SKIN DAMAGED. COMPLIED WITH EC/TC REO 670-53-00-290 AND REO 670-53-00-290, REV D.
FS 333.00 HAS CORROSION AT STR 27 NEED TO BE EVALUATED. REMOVED RIVETS IN FRAME 333 BETWEEN 26L & 26R STARTED BLENDING CORROSION FOUND SEVERE CORROSSION TO BE OUT OF LIMITS REF SRM 51-21-06-001-001-A01 & SRM 51-42-06-001-001-A01. COMPLIED WITH GREO 670-53-21-0799 & EC/TC REO 670-53-21-799 03.
RIGHT ELECTRICAL BAY FLOOR PANEL IS CRACKED BS 193. RECIEVED AND COMPLIED WITH ECTC REO 690-53-11-855 AND REO 690-53-11-855.
MULTIPLE CORRODED FASTENERS ALONG STR 25R BETWEEN FS 319.00 AND 333.00 NEED TO BE EVALUATED. R & R AFFECTED FASTNERS AND CLEAN AREA. REMOVED FASTENERS STR 25R BETWEEN FS 319 AND FS 333 BLENDED CORROSION FOUND SEVERE PITTING IN STR 25R SPLICE & STR 25R REF SRM 53-21-03-101-002-A02 AND SRM 51-42-06-001-001. REMOVED, LOCATED & DRILLED HOLES, AND BEGAN INSTALLING STG 25R SPLICE AT FS 333 IAW SRM 51-42-06-001-001 A01, 51-40-11-001-001 A01. LOCATED & DRILLED HOLES AND BEGAN INSTALLING STR 25R BETWEEN FS 280-333 IAW SRM 51-42-06-001-001, A01 51-40-11-001-001 A01. FINISHED INSTALLING STR SPICE IAW SRM 51-42-06-001-001-A01, DWG S4670-32420. FINISHED INSTALLING STR 25R IAW SRM 51-42-06-001-001 A01, DWG SH670-31630.
RT AFT EMERGENCY EXIT FAILED FUNCTIONAL CHECK, PULLED 60LBS MAX IS 40. CLEARED AND APPLIED NEW GREASE TO SHOOT BOLT SHOOTBOLT FITTING ON RT AFT EMERGENCY EXIT AND THEN IT PASSED FUNCTIONAL TEST IAW AMM 52-21-00-720-802 A01.
CRAWLWAY FLOOR SUPPORT ANGLE HAS CORROSION AT BS 280. REMOVED FLOOR SUPPORT ANGLE RECEIVED & DRILLED UP NEW ANGLE & INSTALLED 3 EA NUTPLATES REF SRM 51-42-06-001-001 & DWG CC670-34256. INSTALLED SERVICEABLE FLOOR SUPPORT ANGLE REF SRM 51-42-06-001-001 & DWG CC670-34256.
FS 280 BUTTSTRAP HAS CORROSION FROM STR 25R-22R. REMOVED CORROSION AT DISCREPANT LOCATON REF: SRM 51-21-06-001-001-A01 FURTHER EVALUATION REQUIRED. PERFORMED UT THICKNESS INSP IAW BSC NDTM SECTION 4.3 MIN REMAINING THK IS .048" ORIGINAL IS .080" REMOVED IS .032" PERFORMED EDDY CURRENT INSP IAW NDTM PT 1, 51-20-006-250-A01, NO INDICATIONS NOTED AT THIS TIME. REMOVED 51EA SOLID RIVETS FROM BUTT STRAP AT FS 280.00 BETWEEN STR 25R-22R, REF: SRM 51-42-06-001-001 A01. INSTALLED NEW RIVETS, 51 EA, IN BUTTSTRAP AT FS 28.00 BETWEEN STR 25R-22R, REF: SRM 51-42-06-001-001-A01. COMPLIED WITH STS EA 32-2016-030 PRINTED 3/7/2016. RECEIVED AND COMPLIED WITH EC/TC EA 32-2016-030, REV D.
FWD INTERCOSTAL AT STR 26R, NEAR AVIONICS DOOR SUROUND IS CORRODED NEED TO BE EVALUATED. R & R INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 DWG SH 670-32077 AND STR 26R BETWEEN TW FS 349 AND 364.
LEFT ELECTRICAL BAY FLOOR IS CRACKED FS 193.00. REPAIRED CRACK IN FS 193 ELECTRICAL BAY FLOOR LT SIDE OR RT SIDE IAW REO 670-53-11-509, REV C LT SIDE ONLY.
EMERGERNCY EXIT SIGN COVER CRACKED SEAT 1A. REMOVED EMERGENCIES EXIT SIGN AT SEAT IA IAW AMM 35-51-05-000-801, A13. INSTALLED NEW EMERGENCY EXIT SIGN AT SEAT 1A IAW AMM 33-51-05-400-801 A13.
FS 310.00 HAS CORROSION AT STR 27 NEED TO BE EVALUATED. REMOVED RIVETS AT FS 310.00 26L-25R BLENDED CORROSSION FOUND SEVERELY CORRODED THRU ATTACH FLANGE FOUND OUT OF LIMITS REF SRM 51-21-06-001-001 AND SRM 51-42-06-001-001. C/W GREO 670-53-21-0799 AND EC/TC REO 670-53-21-799 01. FABRICATED REPAIR SPLICE ANGLES IAW EC/TC REO 670-53-21-799 01. COMPLIED WITH HEAT TREAT OF SPLICE ANGLES IAW SRM 51-24-06-001-001-A01.
FS 295.00 HAS CORROSION AT STR 27 & 25R NEED TO BE EVALUATED. REMOVED CORROSION COMMON TO DISCREPANT AREA REF SRM 51-21-06-001-001-A01 FOUND DAMAGE TO BE OUT OF LIMITS AT BOTH LOCATIONS IAW SRM 53-21-06-101-002-A02. REPAIR DAMAGED AREAS WITH FRAME SPLICE REPAIR REF SRM 53-00-06-201-001-A03. SRM REPAIR REQUIRES DEVIATION AND IS NOT APPLICABLE. COMPLIED WITH GREO 670-53-21-0799 AND ECTC REO 670-53-21-799. FABRICATED REPAIR SPLICE ANGLES IAW EC/TC REO 670-53-21-799. COMPLIED WITH HEAT TREAT OF SPLICE ANGLES IAW SRM 51-24-06-001-001-A01.
RIGHT FWD EMERGENCY EXIT FLOOR LIGHT STRIP NOT INSTALLED. INSTALLED RT FWD EMERGENCY FLOOR EXIT STRIP IAW AMM 33-51-01.
MEGAPHONE DOES NOT WORK. R & R MEGAPHONE IAW AMM 25-61-14. AIPC REF 25-61-14 FIG 1K, ITEM 5.
FWD CARGO DOOR LOWER SEAL RETAINER DAMAGED. BLENDED OUT GOUGES TO A SMOOTH CONTOUR, FWD AND AFT SIDES, DRESS BACK SEAL RETAINER TO WITH-IN .050" OF ORIGINAL PROFILE. ALL WORK ACCOMPLISHED IAW REO 690-52-35-013, REV A. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3. TOUCHED UP RE-WORKED AREAS AND ENSURED SEAL IS PROPERLY SUPPORTED AND RETAINED IN POSITION IAW REO 690-52-35-013, REV A.
CENTER CARGO DOOR LOWER SEAL RETAINER DAMAGE. CBLENDED OUT GOUGES TO A SMOOTH CONTOUR, FWD AND AFT SIDES- DRESS BACK SEAL RETAINER TO WITHIN .050" OF ORIGINAL PROFILE. ALL WORK ACCOMPLISHED IAW REO 690-52-35-013 REV A. TOUCHED UP REWORKED AREAS AND ENSURED SEAL IS PROPERLY SUPPORTED AND RETAINED IN POSITION IAW REO 690-52-35-013, REV A. MAJOR REPAIR IAW GMM 5-3.
LEFT SIDE OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LT SIDE LIGHT OVERWING ASSY IAW AMM 33-51-15, 33-51-15, FIG 1, ITEM 22. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTICED. OK FOR SERVICE.
EXIT SIGN INOP AT RT AFT EMERGENCY EXIT DOOR. TROUBLESHOT AND FOUND WIRE PULLED OUT OF CONNECTOR P860, REPAIRED CONNECTOR IAW WDM 33-50-11 EMERGENCY LIGHTS. OPS CHECKED GOOD AT THIS TIME IAW AMM 33-51-00-710-802.
LT SIDE SEAT TRACK CORRODED AT FS 672-722. REMOVED & REPLACED IAW AMM 53-00-49-000-801 & AMM 53-00-49-400-801.
LEFT OVERWING EXIT LIGHTS HAVE BROKEN WIRES. REMOVED LIGHT IAW AMM 33-51-15-000-801. INSTALLED SERVICEABLE LIGHT IAW AMM 33-51-15-400-801. OPS CHECKED IAW AMM 33-51-15-710-801. OPS CHECKED GOOD.
RIGHT OVERWING EXIT LIGHT FWD HAS BROKEN WIRES. REMOVED LIGHT IAW AMM 33-51-15-000-801. INSTALLED SERVICEABLE LIGHT IAW AMM 33-51-15-400-801. OPS TESTED IAW AMM 33-51-15-710-801, NO DEFECTS FOUND. REPAIRED GROUND WIRE IAW ESPM 20-16-05.
SEAT TRACK BS 743 -763 FOUND CORRODED OUT OF LIMITS IAW SRM 53-51-49-101-001. R & R SEAT TRACK IAW AMM 53-00-49-000-801, AND 53-00-49-400-801.
LT SIDE SEAT TRACK AT FS 483 - 661+14 CORRODED BEYOND LIMITS IAW SRM 53-51-44-101-001. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801.
SEAT TRACK BS 784 - 847+14 CORRODED OUT OF LIMITS IAW SRM 53-51-49-101-001. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A07 & 53-00-49-400-801-A07.
SEAT TRACK BS 897+14 - 907 CORRODED AND IS OUT OF LIMITS IAW SRM 53-51-49-101-001. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801 AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.
FUSELAGE FRAME FS 349 AFT STRINGER 26L - 26R CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001 AND SRM 53-21-06-101-006-A02 .003 BEYOND ALLOWED LIMITS.
RT FLOORBEAM CORRODED AT FS 280. COMPLIED WITH SRM REPAIR 53-21-43. FABRICATED AND INSTALLED A DOUBLER AND A FILLER IAW SRM 53-21-43-201-002-A01, PARA 5.B. MAJOR REPAIR.
SEAT TRACK BS 469-581 CORRODED IN SEVERAL PLACES. R & R SEAT TRACK IAW AMM 53-00-49-400-801 A09 53-00-49-000-801 A09.
RT SIDE SEAT TRACK FROM BS 661-669 CORRODED IN SEVERAL PLACES. REMOVED RT SIDE SEAT TRACK IAW AMM 53-00-49-000-801. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801.
SEAT TRACK BS 785.15 - 847+16 CORRODED IN SEVERAL PLACES. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801(A07) AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801(A01).
SEAT TRACK BS 744.15 - 761.85 CORRODED IN SEVERAL PLACES. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801, CONFIG A07 AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.
RT SIDE SEAT TRACK FROM FS 847+16-865 CORRODED IN SEVERAL PLACES. REPLACED SEAT TRACK IAW AMM 53-00-49-400-801.
SEAT TRACK BS 669.4 - 720.85 CORRODED IN SEVERAL PLACES. R & R SEAT TRACK IAW AMM 53-00-46-000-801 & 53-00-49-400-801.
SEAT TRACK BS 469-581 CORRODED IN SEVERAL PLACES. R & R SEAT TRACK IAW AMM 53-00-49-000-801 A01.
FLOOR PANELS 195DL AND 196DR INTERCONNECT STRAP IS CRACKED IN HALF. COMPLIED WITH REO 690-53-882-049. MAJOR REPAIR.
FS 364 INTERCOSTAL JUST LEFT OF STRINGER 27 IS CORRODED ON THE VERTICAL AND HORIZONTAL LEGS. UPON FURTHER EVALUATION FOUND CORROSION TO WEB ATTACH FLANGE, NO DAMAGE ALLOWED IN AREA OF LATCH PIN INTERCOSTAL IAW SRM 53-21-23-101-003-A01. REMOVED LATCH PIN INTERCOSTAL IAW SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. LOCATED AND DRILLED INTERCOSTAL LOCATED JUST LT OF STRINGER 27 IAW DWG NR SH670-32050. MAJOR REPAIR.
FS 364 INTERCOSTAL JUST RIGHT OF STRINGER 27 IS CORRODED ON THE VERTICAL AND HORIZONTAL LEGS. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. REMOVED LATCH PIN INTERCOSTAL IAW SRM 51-42-21-001-001-A01 AND 51-42-06-001-001A-01. LOCATED, DRILLED AND BEGAN INSTALLATION OF NEW INTERCOSTAL INSTALLED LOCK FASTENERS AND TWO RIVETS IAW SRM 51-42-21-001-001 AND SRM 51-42-06-001-001-A01.
LEFT SIDE SEAT TRACK FROM BS 379-669.4 CORRODED IN SEVERAL PLACES. R & R IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
BS 280 FLOORBEAM CORRODED ON LT AND RT SIDES COMING FROM BETWEEN BEAM AND SACRIFICIAL PLATE AND BEAM IN MULTIPLE LOCATIONS. REMOVED AND INSTALLED SERVICEABLE FS280 RT FLOOR SUPPORT BEAM IAW SRM 51-42-06-001-001-A01, 51-42-21-0001-001-A01, 51-42-10-001-001-A01 AND DWG 16170. MAJOR REPAIR.
LT SEAT TRACK FROM FS 669.4 - 977 CORRODED IN SEVERAL PLACES. R & R IAW AMM 53-00-419-000-801 & 53-00-49-400-801.
SEAT TRACK BS 669.4 - 977 CORRODED IN SEVERAL PLACES. REPAIRED IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.
SEAT TRACK FROM BS 379-669.4 CORRODED IN SEVERAL PLACES. REPAIRED IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.
BS 280 CIRCUMFERENTIAL FRAME STRAP CORRODED BETWEEN 25L-26R. REMOVED CORROSION IAW SRM 51-21-06-001-001. RECEIVED REO PL 690-53-21-587 AND COMPLIED WITH REPAIR. MAJOR REPAIR.
RT AFT EMERGENCY DOOR EXIT HAS MISSING EMERGENCY FLOOR LIGHT STRIP. REPLACED RT AFT EMERGENCY DOOR EXIT EMERGENCY FLOOR LIGHT STRIP IAW AMM 33-51-01.
SEAT 16C IS MISSING LIFE VEST. SEAT 1C & 7B LIFE VEST HAS HOLES IN BAG. REMOVED AND REPLACED 1C AND 7B LIFE VEST AND REPLACED 16C IAW AMM 25-16-03.
FLIGHT OBSERVER LIFE VEST TORN. REMOVED AND REPLACED FLIGHT OBSERVER LIFE VEST IAW AMM 25-61-03.
OVERHEAD CABIN EMERGENCY LIGHTS NOT ILLUMINATING. REMOVED AND REPLACED NR 4 EMERGENCY LIGHTS POWER SUPPLY AND COMPLIED WITH OPS CHECK IAW CRJ900 AMM 33-50-00. NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE.
EMERGENCY LIGHTS WILL NOT TURN OFF. REMOVED AND REPLACED OPS CHECK OF EMERGENCY BATTERY PACK IAW CRJ 900 AMM 33-51-17. REF CONTINUATION FOR DETAILS NO DEFECTS NOTED.
NR 3 LEFT AISLE SEAT TRACK CORRODED. REPAIRED IAW BOMBARDIER AMM 53-00-49.
RIGHT AISLE NR 1 SEAT TRACK CORRODED. REPAIRED IAW AMM 53-00-49.
RIGHT AISLE NR 2 SEAT TRACK CORRODED. REPAIRED IAW AMM 53-00-49.
LEFT AISLE NR 4 SEAT TRACK CORRODED. REPAIRED IAW AMM 53-00-49.
RIGHT AISLE NR 4 SEAT TRACK CORRODED. REPAIRED IAW AMM 53-00-49.
RIGHT INBOARD FLAP DAMAGED. REPAIRED IAW BOMBARDIER REO 670-57-52-160.
LEFT FORWARD EMERGENCY EXIT DOOR LINER IS DAMAGED AT LOWER AFT CORNER. REPAIRED LEFT FORWARD EMERGENCY EXIT DOOR LINER. DAMAGE AT LOWER AFT CORNER IAW C&D ZODIAC PROCEDURE MANUAL 25-6000-1 PG 6037 PARA (D).
FOUND FS 280 BULKHEAD WEB CORRODED. REPAIRED IAW BOMBARDIER REO 670-53-11-594.
FLOORBEAM AT LBL12 FORWARD OF FS280 CRACKED. REPAIRED IAW BOMBARDIER REO 690-53-11-431.
EMERGENCY LIGHT STRIP IN GALLEY MISSING. INSTALLED EMERGENCY LIGHT STRIP IN GALLEY IAW WITH CMM 33-51-01.
LIFE VEST PLACARD LOCATED UNDER SEAT ON TRAY TABLE DAMAGED AT SEAT 6D. REPLACED LIFE VEST PLACARD AT SEAT 6D PER AMM 11-30-04. OK FOR SERVICE.
13CD EMERGENCY LIGHT MISSING. INSTALLED EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD.
AILERON TRIM SWITCH INOP- (IN CENTERED POSITION). REMOVED AND REPLACED AILERON TRIM SWITCH IAW CRJ 900 ESPM 20-45-15. OPS CHECK GOOD OK FOR SVC. DM CLEARED PLACARD REMOVED.
RIGHT BRAKE FEELS STICKY. INSPECTED RT OUTBD ASSY ACTIVATED BRAKE. NO DEFECTS NOTED IAW CRJ 900 AMM 32-40-00. A/C OK FOR SERVICE AT THIS TIME.
RT MAIN BRAKES FEEL SPONGY AND REDUCED BRAKING ACTION ON RT SIDE. BTMS TEMP ON RT I/B BRAKE IS 2 VERSUS 7 ON RT OUTBOARD BRAKE. (LT BTMS 4 ON IB AS WELL AS O/B). BLED NR 3 HYD SYS IAW CRJ-900 AMM 32-43-00. OPS CHECKED GOOD. OK FOR SERVICE. LEAKS CHECKED GOOD. DURING T/S, FOUND NR 3 BRAKE ACCUMULATOR GAUGE BAD. REMOVED AND REPLACED NR 3 BRAKE ACCUMULATOR GAUGE IAW CRJ-900 AMM 32-43-30, OPS AND LEAKS CHECKED GOOD. OK FOR SVC. P/N EFFECTIVITY VERIFIED.
RT BRAKE IS VERY SPONGY. PETAL GOES ALMOST TO THE FLOOR BEFORE BRAKING. BTMS READS 7 ON OUTBOARD. INBOARD INDICATES NORMAL. PERFORMED OPS CHECK OF BRAKING SYSTEM. REF CRJ 900 AMM 32-43-00. CHECKS GOOD. OK FOR SERVICE.
ASYMETRIC BRAKING DURING LANDING RT O/B BTMS 12 OTHERS 3. REMOVED AND REPLACED RIGHT OUTBOARD BRAKE UNIT ASSY. LEAK AND OPS CHECKED GOOD PER CRJ-900 AMM 32-43-26. PART EFFECTIVITY VERIFIED.
TCAS ANTENNA DOUBLER AT FS 295-310 S26R TO S-26L FOUND CORRODED. REPAIRED IAW SRM 51-42-06.
ABORTED TAKEOFF FOR AILERON TRIM PERFORMED INSP OF POSITION TRANSMITTERS IAW AMM 27-15-15 & OPS CHECK OF AIL TRIM SYSTEM IAW AMM 27-11-00, NO DEFECTS NOTED.
SULPHUR LIKE ODOR DETECTED POST LANDING WITH HAZE PRESENT IN FLIGHT DECK AND CABIN. CREW SELECTION OF LT AND RT PACK TO OFF. STOPPED ON THE TAXI-WAY. INFORMED ATC AND PREPARED AIRCRAFT FOR EVACUATION. ATC ALERTED FIRE/RESCUE. EVACUATION NOT REQUIRED. TAXI TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE ISOLATED TO FAULTY LT PACK. LT PAC DEFERRED IAW MEL 21-51-11.
OUTER HANDLE ASSEMBLY OF THE PASSENGER DOOR WAS BROKEN OFF. THE FORWARD AND AFT DOOR SIDE CLOSURE PANELS SUSTAINED SLIGHT BUCKLING, THE INTERNAL PULLEY BRACKETS WERE DAMAGED, AND THE OUTER LOWER DOOR SKIN WAS SCUFFED. FERRY FLY AIRCRAFT TO MX FACILITY IAW EA 09-2011-028 WHERE THE DOOR HANDLE WILL BE REPLACED AND THE DOOR WILL BE PERMANENTLY REPAIRED.
FOUR LOCATIONS OF SCRATCH/GOUGE DAMAGE WERE FOUND ON THE MAIN PASSENGER ENTRY DOOR OUTER SKIN. THE LARGEST DAMAGE AREA MEASURES 0.60 INCH BY 0.20 INCH WIDTH AND A MAXIMUM DEPTH OF 0.014 INCH. THE OTHER TWO DAMAGE AREAS ARE APPROXIMATELY 2 INCHES FORWARD OF THE DOOR AFT EDGE AND ARE 0.35 INCH BY 0.10 INCH WIDE WITH A MAXIMUM DEPTH OF 0.009 INCH. TEMPORARY REPAIR AND FLY ON FOR 6000 FH IAW STS ENGINEERING EA 5-2010-184 WITHIN WHICH TIME A PERMANENT REPAIR MUST BE COMPLETED.
ON CLIMBOUT, FUEL CHANNEL 1 FAIL STATUS MSG, THEN AUTO XFLOW INHIB, THEN XFLOW PUMP CAUTION MSG. ALL GAUGES INOP. ON DESCENT, GOT THE CONTROL & RIGHT FUEL GAUGES. REMOVED AND REPLACED FQGC IAW CRJ 900 AMM 28-41-22. OPS CHECK GOOD, OK FOR SERVICE.
AIR RETURN FOR EXTERNAL ELECTRICAL/COM PANEL LEFT OPEN BY GROUND CREW. INSPECTED & OPS CHECK EXT ELEC/COMM PANEL & DOOR WITH NO DEFECTS. REF CRJ900 AMM 24-20-00.
DURING CLIMB-OUT FROM KMEM, THE COCKPIT AND CABIN FILLED WITH SMOKE. THE FLIGHT CREW DONNED O2 MASKS, COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY WITH ATC. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE. THE AIRCRAFT WAS STOPPED ON THE TAXIWAY AND CFR INSPECTED THE AIRCRAFT. THE PASSENGERS WERE REMOVED AND TRANSPORTED TO THE TERMINAL ON BUSES. MAINTENANCE DETERMINED THAT THE CAUSE OF THE SMOKE WAS RESIDUAL FLUID FROM THE PREVIOUS NIGHT'S COMPRESSOR WASH. THE AIRCRAFT WAS RUN UP TO TOGA POWER WITH THE BLEEDS ON. NO FURTHER SMOKE, FUMES OR VAPORS WERE DETECTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. PINNACLE AIRLINES IS REVIEWING THE COMPRESSOR WASH PROCEDURE TO DETERMINE IF THE PROCESS SHOULD BE MODIFIED TO PREVENT FUTURE EVENTS.