Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR I5EA2021011900006Battery Pack · no testR1 EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BATTERY PACK M1674. OPERATIONS CHECK GOOD, IAW B737-400 AMM 33-51-02.SDR I5EA2020101600006Smoke Detector · false activationINTERMITTENT "MAIN CARGO SMOKE" INDICATION UPON INITIAL DESCENT FOR A FEW MINUTES, THEN NO FURTHER INDICATION. RAN SMOKE DET TEST, PER AMM 10-R-817-MM REV D SUP 26-19-01. TEST GOOD.SDR I5EA2020100500002Slide · unwanted deployL1 DOOR EVACUATION SLIDE INADVERTENTLY DEPLOYED BY GROUND CREW. SLIDE DEFFERED ON LOGPAGE 59980, MEL 52-16, CAT B, EXP 9-16-20, TRACKING NUMBER 2009035. SLIDE REPLACED ON LOGPAGE 59981, IAW B737 AMM 25-61-35.SDR Q2SA20200608432Buss · malfunctionedAIRCRAFT GROUNDED. GEN 1 LOSS TRANSFER BUS FAIL ALL INSTRUMENTS OFF EXCEPT F/O PFD. FOUND GEN CONTROL UNIT #1 UNLOCKED AND SLID OUT OF RACK APPROX 3 IN RESECURED #1 GCU AND PERFORMED OPS CK IAW B737-400 AMM 24-21-81-404-007 AND 24-21-81-705-001 ALL CKS GOODSDR EE4Y2020020210596Fitting · wornSECTION 46 RH STRUT SUPPORT FITTING AFT LUG AT BS 685 WITH WEAR. THE PART WAS REPAIRED IAW BOEING ID #3-4617944374 UNDER 8100-9 FORM AND COOPESA EO COO-EO-2020-10578 R01SDR EE4Y2020020210594Stringer · corrodedAFT CARGO COMPART. STRINGER 26R WITH EXISTING REPAIR LOCATED BTWN S-787 / S-807. THE STRINGER WAS REPAIRED IAW AEI TICKET 10188.SDR EE4Y202002010593Tripler · corrodedAFT CARGO COMPT. DOOR CUT OUT WITH INTERNAL TRIPLER CORRODED LOCATED BTWN STA787 / STA 794.3 AND BTWN S-25R / S-26R. THE MENTIONED PART WAS REPAIRED IAW FROM AEI REF. TICKET 10188.SDR EE4Y202002010590Structure · corrodedLOWER FUSELAGE AFT CARGO COMPT. AT BS 727F BTWN S-27L AND S-27R WITH LOWER SECTION CLIPS CORRODED. THE MENTIONED CLIPS WERE REPLACED.SDR EE4Y202002010589Shear Tie · corrodedLOWER FUSELAGE AFT CARGO COMPT. AT BS 727F BTWN S-27L AND S-26R WITH LOWER SECTION CORRODED. THE MENTIONED PART WAS REPAIRED IAW B737-400 SRM 53-00-07-2R-17 REPAIR 17 FIG. 202 DETAIL V.SDR EE4Y202002010588Shear Tie · corrodedLOWER FUSELAGE AFT CARGO COMPT. AT BS 887 BTWN S-27L AND S-27L WITH LOWER SECTION CORRODED. THE MENTIONED PART WAS REPAIRED IAW B737-400 SRM 53-00-07-2R-17 REPAIR 17 FIG. 202 DETAIL VI.SDR EE4Y202002010585Skin · wornLH WING O/B MID FLAP LOWER SURFACE WITH WEAR AT WBL 255. THE MENTIONED PART WAS REPAIRED IAW BOEING ID #3-4620339317 AND COOPESA E.O. COO-EO-2020-10540-R01SDR Q2SA20190522418Control Panel · shortedAIRCRAFT GROUNDED. ELECTRICAL SMOKE SMELL @ FL 340. MCP FAILED VNAV AND LNAV. ALL INDICATIONS FAILED TO INPUTS. MCP REMOVED AND REPLACED MCP 22-11-34-004-003 AND -004. DFCS MCP BITE TEST GOOD IAW AMM 22-11-34-745-001. ACFT OK FOR SERVICE. PILOT STATED THAT SMSDR EE4Y2018070906891Skin · crackedDURING THE CURRENT MAINTENANCE PROCESS IT WAS FOUND AT FWD ENTRY DOOR AREA, THE FUSELAGE SKIN WITH CRACK AT THE SILL LOWER AFT CORNER. DUE TO THIS SITUATION THE SKIN WAS REPAIRED AS PER SRM 53-10-01 REPAIR 12 FIGURE 201.SDR EE4Y2018070906892Attach Angle · crackedDURING THE CURRENT MAINTENANCE PROCESS IT WAS FOUND AT THE EMPENNAGE, VERTICAL STABILIZER TO FUSELAGE LEFT ATTACHMENT SUPPORT ANGLE CRACKED AT THE BS 1121 FIN WL 0.0. DUE TO THIS SITUATION THE AFFECTED SUPPORT ANGLE WAS REPAIRED AS PER SRM 53-80-71 REPAIR 1, FSDR EE4Y2018070906884Stringer · corrodedDURING THE CURRENT MAINTENANCE PROCESS IT WAS FOUND AT RT WING THE UPPER VENT STRINGERS S9U-S10U WITH CORROSION ON THE CHANNEL AREA INTERNAL SURFACE AT WS 557. THE CORROSION WAS COMPLETELY REMOVED AS PER SRM 51-10-02 PARAGRAPH 14A AND IT WAS FOUND OUT OF LIMIT