N637CZ
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Compass Airlines, LLC | Operator | on 2018-06-16 | Operator named in NTSB report |
Accident & incident history
Operated by Compass Airlines (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
68 reports on file, 2010-09-08 – 2018-12-03.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 26,972 hrs · 16,204 cycles
THIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH THE INSTRUCTIONS THAT ARE SPECIFIC TO THE RH HORIZONTAL STABILIZER FROM SB 170-55-0014, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION THAT CONSISTS OF REPLACING HORIZONTAL STABILIZER RIBS 10A, 11A, AND 12A WITH NEW, REINFORCED RIBS. THIS MODIFICATION IS DESIGNED TO HELP PREVENT POSSIBLE CRACKS ON THE HORIZONTAL STABILIZER CENTER BOX RIBS AND TO REACH THE AIRCRAFT ECONOMICAL FATIGUE LIFE. COMPASS ENGINEERING HAS CLASSIFIED THIS MODIFICATION AS A MAJOR ALTERATION. ONE OR MORE OF THE RIBS THAT ARE BEING REPLACED AS PART OF THE SERVICE BULLETIN WERE FOUND CRACKED DURING AN INSPECTION WHILE AT BASIC CHECK. BY ACCOMPLISHING SB 170-55-0014, THIS EO ALSO PROVIDES A REPAIR BY REPLACEMENT OF THE AFFECTED RIB(S). COMPASS ENGINEERING HAS CLASSIFIED THIS REPAIR AS A MAJOR REPAIR. THIS EO IS BEING MADE EFFECTIVE TO ALL DELTA AIRCRAFT FOR WHICH SB 170-55-0014 IS APPLICABLE, BUT A MAXIMO EVENT WILL ONLY BE GENERATED FOR AN AIRCRAFT WHEN ONE OR MORE RIBS ARE FOUND CRACKED. THE ACCOMPLISHMENT INSTRUCTIONS OF THIS EO WERE DERIVED FROM EMBRAER SERVICE BULLETIN 170-55-0014; THEREFORE, A COPY OF THIS SB IS NOT NEEDED TO ACCOMPLISH THIS EO.
Part: FITTING — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 26,972 hrs · 16,204 cycles
CORROSION HAS BEEN FOUND ON THE FWD CARGO DOORWAY â FWD FITTING P/N 170-66803-401, CENTER FITTING P/N 170-66804-401, AND/OR AFT FITTING P/N 170-66803-402 ON SEVERAL COMPASS AIRCRAFT DURING BASIC CHECK. SINCE EMBRAER CLASSIFIES THESE FITTINGS AS PSES, COMPASS HAS CLASSIFIED REPLACEMENT OF THESE FITTINGS AS A MAJOR REPAIR. IN LIEU OF CONTINUING TO WRITE INDIVIDUAL EOS FOR EACH AIRCRAFT. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS FOR THE ON CONDITION REPAIR OF CORRODED OR DAMAGED FWD CARGO DOORWAY - FWD, CENTER, AND AFT LOWER SEAL REST FITTINGS BY PART REPLACEMENT. THE REPLACEMENT IS ACCOMPLISHED USING THE EMBRAER PRODUCTION DRAWINGS AND SRM CHAPTER 51 PROCEDURES. SINCE THE DAMAGED STRUCTURE IS BEING REPLACED WITH NEW PARTS PER THE PRODUCTION DRAWINGS, THE AIRCRAFT STRUCTURE REMAINS IN ITS ORIGINAL CONFIGURATION. THEREFORE, NO CHANGES TO THE EXISTING INSPECTION PROGRAM ARE REQUIRED. EO E17X-5300-007 HAS BEEN ACCOMPLISHED FLEETWIDE ON THE AIRCRAFT EFFECTIVE TO THIS EO TO COMPLY WITH SB 170-53-0104 BY ADDING DRAIN HOLES TO THE AFFECTED PARTS FROM THIS REPLACEMENT EO. ADDITIONAL SURFACE PROTECTION AND CIC WAS ALSO ADDED TO PREVENT FUTURE CORROSION IN THE AREA. RELEVANT ACCOMPLISHMENT INSTRUCTIONS FROM EO E17X-5300-007 HAVE BEEN INCLUDED IN THIS EO TO MAINTAIN THE CONFIGURATION OF THE AIRCRAFT. REV 1: IS BEING ISSUED TO INCLUDE ALL E175 FLEET EFFECTIVITY. REV 2: THIS REVISION IS BEING ISSUED TO ADD A STEP BEFORE THE FINAL STEP TO ENSURE AN SDR WAS SUBMITTED FOR THIS REPAIR. REV 3: THIS REVISION IS BEING ISSUED TO ENSURE THE MODIFICATION THAT WAS PREVIOUSLY ACCOMPLISHED BY EO E17X-5300-007 REMAINS COMPLETED ON THE PARTS THAT ARE BEING REPLACED.
Part: ATTACH FITTING — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 26,972 hrs · 16,204 cycles
CORROSION HAS BEEN FOUND ON THE AFT CARGO DOORWAY â FWD FITTING P/N 170-85492-403, CENTER FITTING P/N 170-85251-401, AND/OR AFT FITTING P/N 170-85493-403 ON SEVERAL COMPASS AIRCRAFT DURING BASIC CHECK. SINCE EMBRAER CLASSIFIES THESE FITTINGS AS PSES, COMPASS HAS CLASSIFIED REPLACEMENT OF THESE FITTINGS AS A MAJOR REPAIR. IN LIEU OF CONTINUING TO WRITE INDIVIDUAL EOS FOR EACH AIRCRAFT. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS FOR THE ON CONDITION REPAIR OF CORRODED OR DAMAGED AFT CARGO DOORWAY - FWD, CENTER, AND AFT LOWER SEAL REST FITTINGS BY PART REPLACEMENT. THE REPLACEMENT IS ACCOMPLISHED USING THE EMBRAER PRODUCTION DRAWINGS AND SRM CHAPTER 51 PROCEDURES. SINCE THE DAMAGED STRUCTURE IS BEING REPLACED WITH NEW PARTS PER THE PRODUCTION DRAWINGS, THE AIRCRAFT STRUCTURE REMAINS IN ITS ORIGINAL CONFIGURATION. THEREFORE, NO CHANGES TO THE EXISTING INSPECTION PROGRAM ARE REQUIRED. EO E17X-5300-007 HAS BEEN ACCOMPLISHED FLEETWIDE ON THE AIRCRAFT EFFECTIVE TO THIS EO TO COMPLY WITH SB 170-53-0104 BY ADDING DRAIN HOLES TO THE AFFECTED PARTS FROM THIS REPLACEMENT EO. ADDITIONAL SURFACE PROTECTION AND CIC WAS ALSO ADDED TO PREVENT FUTURE CORROSION IN THE AREA. RELEVANT ACCOMPLISHMENT INSTRUCTIONS FROM EO E17X-5300-007 HAVE BEEN INCLUDED IN THIS EO TO MAINTAIN THE CONFIGURATION OF THE AIRCRAFT. REV 1: IS BEING ISSUED TO INCLUDE ALL E175 FLEET EFFECTIVITY. REV 2: THIS REVISION IS BEING ISSUED TO ADD A STEP BEFORE THE FINAL STEP TO ENSURE AN SDR WAS SUBMITTED FOR THIS REPAIR. REV 3: ENSURE THE MOD THAT WAS PREVIOUSLY ACCOMPLISHED BY EO E17X-5300-007 REMAINS COMPLETED ON PARTS BEING REPLACED. REV 4: THIS REVISION IS BEING ISSUED TO CORRECT AN ERROR IN THE SIGN-OFF STATEMENT
Part: SKIN PANEL — CRACKED (VERTICAL STAB) · airframe 26,972 hrs · 16,204 cycles
DURING BASIC CHECK IN BNA, AN APPROXIMATELY 4.5 INCH LONG CRACK WAS DISCOVERED ON THE VERTICAL STABILIZER RT SKIN JUST AFT OF THE HOISTING POINT. REQUESTED AND RECEIVED PERMANENT REPAIR APPROVAL IN THE FORM OF ETD2018-170-121165 AND ITS CORRESPONDING ANAC DER FORM. THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF THE CRACK DAMAGE LOCATED AT RIB 12 JUST AFT OF THE REAR SPAR ON THE P/N 170-63701-013 RT SKIN OF THE VERTICAL STABILIZER. THE DAMAGE WILL BE REPAIRED BY CUT OUT AND DOUBLER INSTALLATION PER ETD2018-170-121165. BECAUSE THE VERTICAL STABILIZER SKIN IS A PSE AND THIS REPAIR IS RESTORING STRENGTH, ACCOMPLISHMENT OF THIS EO HAS BEEN CLASSIFIED AS A MAJOR REPAIR. THIS IS BEING ACCOMPLISHED BY EO E175-55MR-028.
Earlier reports · 2010–2017 · 64 reports
2017
Part: WIRE HARNESS — FAILED (ANTI ICE SYS) · airframe 24,677 hrs · 14,452 cycles
WING ANTI-ICE LEAK ON CLIMB OUT. FLIGHT UNABLE TO PROCEED TO DESTINATION DUE TO WEATHER CONDITIONS. EMERGENCY DECLARED. MAINTENANCE REMOVED THE NR 4 SLAT ACCESS PANEL IAW AMM 27-83-07 SUBTASK 010-003-A FOR TROUBLESHOOTING. REMOVED AND REPLACED THE LT NR 4 SLAT WING ANTI-ICE BACKWALL TEMPERATURE SENSOR HARNESS IAW AMM 30-11-02. OPS CHECKED GOOD. NO DEFECTS NOTED. INSTALLED SLAT PANEL IAW AMM 27-83-07. ACFT IS OK FOR SERVICE.
Part: FLASHLIGHT — INOPERATIVE (R1 DOOR AREA) · airframe 23,172 hrs · 13,481 cycles
R1 FA FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW T/C 33-51-01-9001-U.
2016
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 21,797 hrs · 12,667 cycles
LEFT AFT F/A FLASHLIGHT INOPERATIVE. REPLACED THE BATTERY IAW AMM 33-51-01.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
FWD CABIN FLOOR CROSSFRAME 16, RT FLOOR SUPPORT, P/N 170-04071-001, IS CORRODED AT Y= 711 X= 4711. REMOVED AND REPLACED CROSSFRAME 16 RT FLOOR SUPPORT IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-198 REV IR.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
AFT CABIN FLOOR CROSSFRAME 90, LT OUTBD GUSSET, P/N 170-60261-001, HAS CORROSION. X= 24868, Y= -520. REMOVED AND REPLACED AFT CABIN FLOOR CROSSFRAME 90 LT OUTBD FLOOR GUSSET IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-197 REV IR.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
FWD CABIN FLOOR CROSSFRAME 17, RT FLOOR SUPPORT, P/N 170-13939-001, IS CORRODED AT Y= 711 X= 5064. REMOVED AND REPLACED CROSSFRAME 17 RT FLOOR SUPPORT IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-198 REV IR.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
FWD CABIN FLOOR LT AFT DOUBLER, P/N 170-07311-001, AT FRAME 19 - 20 HAS CORROSION IN MULTIPLE AREAS AT Y= -538 X=5645 - 6070. REMOVED AND REPLACED LT AFT FLOOR DOUBLER IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-198 REV IR.
Part: SUPPORT RIB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
FWD FUSELAGE FAIRING LOWER SUPPORT RIB ASSY, P/N 170-02456-001, IS CORRODED AT FRAME 45. X=12490, STR 25L - 28L. REMOVED AND REPLACED THE EXTERNAL FUSELAGE FWD WING TO FUSELAGE FAIRING LOWER SUPPORT RIB ASSY IAW SRM 51-41-01 & 51-43-01.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
AFT CABIN FLOOR CROSSFRAME 90, RT OUTBD GUSSET, P/N 170-60259-001, HAS CORROSION. X=24868, Y= +468 TO +623. REMOVED AND REPLACED AFT CABIN FLOOR CROSSFRAME 90 RT OUTBD FLOOR GUSSET IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-197 REV IR.
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
AFT CABIN FLOOR CROSSFRAME 90, RT INBD GUSSET, P/N 170-60257-001, HAS CORROSION. X=24868, Y= +273. REMOVED AND REPLACED AFT CABIN FLOOR CROSSFRAME 90 RT INBD FLOOR GUSSET IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-197 REV IR.
Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
AFT CABIN FLOOR RT PANEL SUPPORT (AFT SILL), P/N 170-86181-005, AT FRAME 88 - 90 HAS CORROSION. X=24048 - 24868, Y= +1037. REMOVED AND REPLACED AFT CABIN FLOOR RT AFT FLOOR PANEL SUPPORT (SILL) IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-197 REV IR.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
FWD CABIN FLOOR LT FWD SILL, P/N 170-03275-005, HAS CORROSION IN MULTIPLE AREAS FROM FRAME 12 - 16 AT Y= -1173 X= 3679 - 4711. REMOVED AND REPLACED LT FWD FLOOR SILL IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-198 REV IR.
Part: RETAINER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
CORROSION ON INTERNAL SIDE OF WASTE BOX BRACKET RETAINERS, P/N 170-86654-003 & 170-86655-003. STA 24048 TO 24458, STR 24R TO 27R. PERMANENTLY REMOVED THE WASTE PAN RETAINERS ON EO E17X-5300-004 REV IR.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
FWD CABIN FLOOR RT FWD SILL, P/N 170-05663-003, HAS CORROSION IN MULTIPLE AREAS FROM FRAME 12 - 14 AT Y= 973, X= 3679 - 4270. REMOVED AND REPLACED RT FWD FLOOR SILL IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-198 REV IR.
Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
AFT CABIN FLOOR- RT PANEL SUPPORT (FWD SILL), P/N 170-92908-001, AT FRAME 84 HAS CORROSION. X= 22847, Y= 1200. REMOVED AND REPLACED AFT CABIN FLOOR RT FWD FLOOR PANEL SUPPORT (SILL) IAW SRM 51-41-01 & 51-43-01 ON WO# 2023298090 PER COMPASS EO E175-5300-197 REV IR WO# 2175750.
Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
AFT CABIN FLOOR CENTER SHEAR PANEL, P/N 170-65928-001, FRAME 87 - 88 HAS CORROSION. X= 23865 - 24048, Y= -222 - +222. REMOVED AND REPLACED AFT CABIN FLOOR CENTER SHEAR PANEL IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-197 REV IR.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
FWD CABIN FLOOR RT AFT SILL, P/N 170-05661-003, HAS CORROSION IN MULTIPLE AREAS FROM FRAMES 17 - 20 AT Y= 1273 X= 5064 - 6070. REMOVED AND REPLACED RT AFT FLOOR SILL IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-198 REV IR.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
FWD CABIN FLOOR LT FWD DOUBLER, P/N 170-12118-001 HAS CORROSION AT FRAME 16. Y= -323, X= 4711. REMOVED AND REPLACED LT FWD FLOOR DOUBLER IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-198 REV IR.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
FWD CABIN FLOOR CROSSFRAME 15, RT FLOOR SUPPORT, P/N 170-04071-001, IS CORRODED AT Y= 711, X= 4520. REMOVED AND REPLACED CROSSFRAME 15 RT FLOOR SUPPORT IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-198 REV IR..
Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
AFT CABIN FLOOR CROSSFRAME 90, LT INBD GUSSET, P/N 170-60257-001, HAS CORROSION. X=24868, Y= -273. REMOVED AND REPLACED AFT CABIN FLOOR CROSSFRAME 90 LT INBD FLOOR GUSSET IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-197 REV IR.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
FWD CABIN FLOOR CROSSFRAME 16, LT FLOOR SUPPORT, P/N 170-13633-001, IS CORRODED AT X=4711 Y= -1115. REMOVED AND REPLACED CROSSFRAME 16 LT FLOOR SUPPORT IAW SRM 51-41-01 & 51-43-01 ON EO E175-5300-198 REV IR.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,787 hrs · 12,662 cycles
THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIR OF CORROSION DAMAGE TO THE UPPER FLANGE OF THE CENTER FUSELAGE III RT BEAM P/N 170-65669-004 AT FR88. THE DAMAGE MEASURES APPROXIMATELY 1 INCH X 1 INCH X 0.013 INCH DEEP. THE PERMANENT REPAIR WILL BE ACCOMPLISHED BY DOUBLER INSTALLATION PER SRM PART II 53-23-10/REPAIR 01P, FIGURE 203. THE SEAT TRACK BEAM IS A PSE, THEREFORE ACCOMPLISHMENT OF THIS EO HAS BEEN CLASSIFIED AS A MAJOR REPAIR DUE TO STRENGTH RESTORATION. THIS IS NOT CLASSIFIED AS FCS AND DOES NOT REQUIRE SUPPLEMENTAL FOLLOW UP INSPECTIONS. THE PERMANENT REPAIR WILL BE ACCOMPLISHED ON WO 2184291.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
FWD CABIN LEFT SEAT TRACK HAS CORROSION AT MULTIPLE LOCATIONS X= 4270 - 5645, BS 273. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-01 & 51-43-01.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 21,787 hrs · 12,662 cycles
RT SEAT TRACK HAS CORROSION X= 3679 - 5645, Y= 273. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-01 & 51-43-01.
Part: SEAT TRACK — CORRODED (FRAME 84) · airframe 21,787 hrs · 12,662 cycles
CORROSION DAMAGE TO THE LT INBOARD SEAT TRACK AT FRAME 84. REPAIRED IAW ETD2016-170-100222.
Part: SEAT TRACK — CORRODED (FRAME 84) · airframe 21,787 hrs · 12,662 cycles
CORROSION DAMAGE TO THE SEAT TRACK FRAME 84. REPAIRED IAW ETD2016-170-100203.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,523 hrs · 12,494 cycles
2L EMER FLASHLIGHT NOT CHARGING. REMOVED AND REPLACED L2 EMER FLASHLIGHT IAW AMM 33-51-01. OPS CHECK GOOD. OK FOR SVC. REMOVED PLACARD SDI SIGNED. MXC NOTIFIED. THIS CLEARS DM2149760. NO FURTHER DEFECTS NOTED.
Part: BATTERY — DISCHARGED (CABIN) · airframe 21,272 hrs · 12,333 cycles
EMERGENCY LIGHT BATTERY FAULT EICAS MSG. RECHARGED EMERGENCY LIGHT BATTERY IAW AMM 33-50-01. OPS CHECK GOOD. OK FOR SERVICE.
2015
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,414 hrs · 10,606 cycles
AFT FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING. R & R AFT FLIGHT ATTENDANT FLASHLIGHT IAW AMM 33-51-01. OK FOR SERVICE.
2014
Part: SKIN — DENTED (FRAME 10) · airframe 16,916 hrs · 9,721 cycles
DENT DAMAGE TO THE FWD FUSELAGE SKIN FWD OF FRAME 10 BETWEEN STRINGERS 17 - 18L. REPAIRED IAW ETD 2014-170-101284, SRM 53-10-01 REPAIR 12P & SRM 51-75-00. MAJOR REPAIR.
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 16,754 hrs · 9,623 cycles
CAPTAIN`S FLASHLIGHT INOPERATIVE. DEFERRED IAW MEL, LATER REPLACED CAPTAIN`S FLASHLIGHT IAW AMM.
Part: FINGER DOUBLER — CORRODED (ZONE 100) · airframe 16,644 hrs · 9,559 cycles
FORWARD CARGO FWD FINGER DOUBLER HAS CORROSION FROM X=7620 TO X=8089 & Y=209 TO Y=400. R & R FWD FINGER IAW SRM 51-41-01 & 51-43-01.
Part: SEAL DEPRESSOR — CORRODED (FUSELAGE) · airframe 16,644 hrs · 9,559 cycles
FORWARD CGO CTR SEAL DEPRESSOR PN 170-66804-401, HAS CORROSION AT X=7938 TO X=8563 STRINGER 26R. R & R LOWER CTR SEAL DEPRESSOR IAW SRM 51-41-01 & 51-43-01 ON WORK ORDER 14752221B9 IAW COMPASS EO E175-53MR-108 REV 2 WO WORK ORDER 1486658.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,852 hrs · 9,116 cycles
FORWARD EMER LIGHT NOT TESTING. R & R FWD LT ELPU IAW AMM. OPERATIONS CHECKED NORMAL.
Part: PRESSURE SWITCH — INTERMITTENT (BRAKE SYSTEM) · airframe 15,439 hrs · 8,879 cycles
PARKING BRAKE ON LIGHT ILLUMINATED INTERMITTENTLY ON APPROACH. LANDING & TAXI OPERATIONS NORMAL. MSG REMAINS CLEARED. IAW FIM TASK 32-41-00-810-852A. CKD PKG BRAKE SWITCH ELEC CONNS, NO DEFECTS NOTED. OPERATIONS CHECKED GOOD IAW AMM 32-44-09 TRANSITORY COND OF PKG BRAKE SWITCH. RESET POWER IAW AMM 24-42-02 AS PRECAUTIONARY, OK FOR SERVICE. FOLLOWING RTS, EMERGENCY BRAKE LIGHT INTERMITTENT ON TAXI WITH INTERMITTENT EMERGENCY BRAKE FAULT. REPLACED EMERGENCY BRAKE PRESS SWITCHES IAW AMM 32-44-09. LEAK & FUNCTIONAL CHECK GOOD. NO FAULT MSG DISPLAYED.
Part: PRESSURE SWITCH — INTERMITTENT (BRAKE SYSTEM) · airframe 15,439 hrs · 8,879 cycles
PARKING BRAKE ON LIGHT ILLUMINATED INTERMITTENTLY ON APPROACH. LANDING & TAXI OPERATIONS NORMAL. MSG REMAINS CLEARED IAW FIM TASK 32-41-00-810-852A. CKD PKG BRAKE SWITCH ELEC CONNS, NO DEFECTS NOTED. OPERATIONS CK GOOD IAW AMM 32-44-09 TRANSITORY COND OF PKG BRAKE SWITCH. RESET POWER IAW AMM 24-42-02 AS PRECAUTIONARY. OK FOR SERVICE FOLLOWING RTS, EMERGENCY BRAKE LIGHT INTERMITTENT ON TAXI WITH INTERMITTENT EMERGENCY BRAKE FAULT. REPLACED EMERGENCY BRAKE PRESS SWITCHES IAW AMM 32-44-09. LEAK & FUNCTIONAL CHECK GOOD. NO FAULT MSG DISPLAYED.
2013
Part: SKIN — DAMAGED (FUSELAGE) · airframe 12,435 hrs · 7,108 cycles
DAMAGE WAS FOUND UNDER THE FOâS SIDE WINDOW ON THE SIDE OF THE FUSELAGE. THE DAMAGE IS A DENT LOCATED BETWEEN FR 05 AND FR 06 AND STGR 21R AND 22R. FORWARD SIDE OF DENT IS LOCATED 5" AFT OF FR 05 AND AFT SIDE OF DENT IS LOCATED 11.10" AFT OF FR 05. THE BOTTOM SIDE OF DENT IS LOCATED 0.05 INCHES ABOVE STGR 22R AND TOP SIDE OF DENT IS LOCATED 1.0 INCH BELOW STGR 21R. THE DENT HAS THE FOLLOWING DIMENSIONS: H = 0.138", W = 6.10" AND L = 3.90".
2012
Part: SUPPORT BRACKET — CORRODED (ZONE 200) · airframe 11,016 hrs · 6,339 cycles
AFT CABIN LT FLOOR SUPPORT AT FR 86 LT SIDE IS BROKEN X=23453 Y=-717.6. R & R LT FLOOR SUPPORT IAW SRM 51-41-01 AND 51-43-01.
Part: GUSSET — CORRODED (ZONE 200) · airframe 11,016 hrs · 6,339 cycles
AFT CABIN RT INBD GUSSET, AT FR 90 HAS CORROSION X=24868 Y= 293. R & R RT INBD GUSSET IAW SRM 51-41-01 AND 51-43-01.
Part: FINGER DOUBLER — CORRODED (ZONE 100) · airframe 11,016 hrs · 6,339 cycles
FWD CARGO THRESHOLD STRUCTURE AFT FINGER DOUBLER, HAS CORROSION AND IS GOUGED FROM X=8463.2 TO X=8843.2 AND Y=300 TO 390. R & R AFT FINGER DOUBLER IAW SRM 51-41-01 AND 51-43-01.
Part: CROSSBEAM — CORRODED (ZONE 200) · airframe 11,016 hrs · 6,339 cycles
FRAME 17, CROSSBEAM, HAS CORROSION X=5064.0 Y=-965.9. FABRICATED REPAIR ANGLE IAW ETD 2012-170-015258-A AND INSTALLED IAW SRM 51-41-01 AND 51-43-01.
Part: UPPER SHEET — CORRODED (ZONE 200) · airframe 11,016 hrs · 6,339 cycles
RT UPPER SHEET, BETWEEN FR 85 & 86 HAS CORROSION X=23453 Y= 272. R & R RT UPPER SHEET IAW SRM 51-41-01 AND 51-43-01.
Part: SILL — CORRODED (ZONE 200) · airframe 11,016 hrs · 6,339 cycles
RT FWD SILL, HAS CORROSION X=4270 Y=1143. R & R RT FWD SILL IAW SRM 51-41-01 AND 51-43-01.
Part: SEAL DEPRESSOR — CORRODED (ZONE 100) · airframe 11,016 hrs · 6,339 cycles
FWD CARGO DOOR LWR-FWD SEAL DEPRESSOR CORRODED AT FR24 X=7918.2 TO 7658.2 STR 26R. R & R LWR-FWD SEAL DEPRESSOR IAW SRM 51-41-01 AND 51-43-01.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 11,016 hrs · 6,339 cycles
AFT CABIN RT FLOORBEAM HAS CORROSION AT FR 87 X=23865 Y= 260.4. R & R RT FLOORBEAM IAW SRM 51-41-01 AND 51-43-01.
Part: FIREWALL — CORRODED (APU BAY) · airframe 11,016 hrs · 6,339 cycles
APU FIREWALL PANEL 351BZ, UPPER FLANGE IS CRACKED 0.350" & LOWER FLANGE IS CRACKED 0.340". BOTH CRACKS ROUTED OUT AND NDT PERFORMED VERIFYING NO MORE CRACKING EXISTS.
Part: FINGER DOUBLER — DAMAGED (ZONE 100) · airframe 11,016 hrs · 6,339 cycles
FWD CARGO THRESHOLD STRUCTURE FWD FINGER DOUBLER, IS GOUGED AND HAS CORROSION AT FR25 Y=310 X=8038.2 REMOVED CORROSION AND BLENDED GOUGE AND TREATED IAW SRM 51-10-03 & 51-12-01.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 11,016 hrs · 6,339 cycles
FWD CABIN LT FLOORBEAM, HAS CORROSION AT FRAME 16, X=4711 Y=-260.4. R & R LT FLOORBEAM IAW SRM 51-41-01 AND 51-43-01.
Part: DOUBLER — CORRODED (ZONE 200) · airframe 11,016 hrs · 6,339 cycles
LT AFT DOUBLER, HAS CORROSION AT FRAME 19 X=5645 Y=736.6. R & R LT AFT DOUBLER IAW SRM 51-41-01 AND 51-43-01.
Part: THRESHOLD — CORRODED (ZONE 100) · airframe 11,016 hrs · 6,339 cycles
FWD CARGO THRESHOLD FLOOR SUPPORT, HAS COOROSION Y=400 X=8038.2. R & R THRESHOLD FLOOR SUPPORT IAW SRM 51-41-01 AND 51-43-01.
Part: SEAL DEPRESSOR — CORRODED (ZONE 100) · airframe 11,016 hrs · 6,339 cycles
FWD CARGO DOOR LWR-AFT SEAL DEPRESSOR, HAS CORROSION BETWEEN X=8843.2 TO 8583.2 STR.24-26R. R & R LWR-AFT SEAL DEPRESSOR IAW SRM 51-41-01 AND 51-43-01.
Part: GUSSET — CORRODED (ZONE 200) · airframe 11,016 hrs · 6,339 cycles
AFT CABIN RT OTBD GUSSET, HAS CORROSION X=24868 Y= 575. R & R RT OTBD GUSSET IAW SRM 51-41-01 AND 51-43-01.
Part: PANEL — CORRODED (ZONE 200) · airframe 11,016 hrs · 6,339 cycles
CENTER SHEAR PANEL, IS CORRODED BETWEEN FR 87 & 88. X=23956.5 Y=-65. R & R CENTER SHEAR PANEL IAW SRM 51-41-01 AND 51-43-01.
Part: PANEL — CORRODED (ZONE 200) · airframe 11,016 hrs · 6,339 cycles
AFT CABIN RT SHEAR PANEL, AT FR 87 HAS CORROSION ALONG FWD EDGE OF PANEL X=23865 Y= 630. R & R RT SHEAR PANEL IAW SRM 51-41-01 AND 51-43-01.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 11,016 hrs · 6,339 cycles
RT FLOORBEAM, HAS CORROSION AS MARKED BETWEEN FRAME 16 AND 17 X=4887.5 Y= -330.2. R & R RT FLOORBEAM IAW SRM 51-41-01 AND 51-43-01.
Part: SEAL DEPRESSOR — CORRODED (ZONE 100) · airframe 11,016 hrs · 6,339 cycles
FWD CARGO DOOR LWR-CENTER SEAL DEPRESSOR, HAS CORROSION BETWEEN X=8038.2 - 8463.2 STR.26. R & R LWR-CENTER SEAL DEPRESSOR IAW SRM 51-41-01 AND 51-43-01.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 10,026 hrs · 5,760 cycles
EMERGENCY LIGHTS AT VARIOUS LOCATIONS, REMAIN ON. LIGHTS CAME ON PRIOR TO LANDING.
Part: SKIN — DENTED (ZONE 200) · airframe 12,435 hrs · 7,108 cycles
DURING A TURN IN MSP, DAMAGE WAS FOUND UNDER THE F/OâS SIDE WINDOW ON THE SIDE OF THE FUSELAGE. THE DAMAGE IS A DENT LOCATED BETWEEN FR 05 AND FR 06 AND STGR 21R AND 22R. FORWARD SIDE OF DENT IS LOCATED 5" AFT OF FR 05 AND AFT SIDE OF DENT IS LOCATED 11.10" AFT OF FR 05. THE BOTTOM SIDE OF DENT IS LOCATED 0.05" ABOVE STGR 22R AND TOP SIDE OF DENT IS LOCATED 1.0" BELOW STGR 21R. THE DENT HAS THE FOLLOWING DIMENSIONS: H = 0.138", W = 6.10" AND L = 3.90".
Part: SKIN — DENTED (FUSELAGE) · airframe 12,435 hrs · 7,108 cycles
A DENT WAS FOUND UNDER THE FOâS SIDE WINDOW ON THE SIDE OF THE FUSELAGE. BETWEEN FR 05 - 06 AND S21R AND 22R.
2011
Part: TRANSMITTER — MALFUNCTIONED (OIL PRESSURE) · airframe 7,301 hrs · 4,255 cycles
IN CRUISE AT FL 230, EICAS DISPLAY ENG 1 LOW OIL PRESSURE, PERFORMED QHR PROCEDURE ON PG 6.7. OIL QTY, TEMP, N1 AND N2 ALL NORMAL - INSPECTED OIL CAP FOR SECURITY. CK'S GOOD. INSPECTED NR1 ENG COWLING, INLET & EXHAUST FOR EVIDENCE OF OIL LEAKAGE, NONE NOTED. INSPECTED INTERIOR ENG COMPONENTS FOR EVIDENCE OF LEAKAGE, NONE NOTED. CMC INDICATES ACTIVE FAULT 73217705CMC, ENG LOW OIL PRESS EICAS EXCEEDANCE DISPLAYED. TROUBLESHOT TO OIL PRESSURE TRANSMITTER. R & R SAME.
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 6,785 hrs · 3,950 cycles
R2 DOOR EMERGENCY LIGHT INOP. R & R AFT OTBD EMERG LIGHT POWER UNIT IAW AMM 33-50-01. OK FOR SVC.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 5,856 hrs · 3,445 cycles
AFT EMERGENCY LIGHTS WILL NOT ILLUMINATE DURING FA TEST. R&R AFT RT AND AFT LT ELPU'S IAW AMM 33-50-01 OPS CHECK GOOD. PART NUMBERS ON 3400-22-10.
2010
Part: WARNING MESSAGE — ILLUMINATED (EMERGENCY LIGHT) · airframe 5,352 hrs · 3,146 cycles
EMERGENCY LIGHT BATTERY FAULT MESSAGE.
Part: POWER UNIT — FAILED (EMERGENCY LIGHTS) · airframe 4,985 hrs · 2,920 cycles
EMERGENCY LIGHTS WOULD NOT TURN ON. POWER UNIT FAILED.