N54241

Service difficulty reports · 117

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N54241' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA2026012913425Stringer · corrodedAFT CARGO AREA, FOUND ADDITIONAL CORROSION ON STRINGER 22R, BS 887. MAJOR REPAIR. DIP LPS 7747663 & 7747714. WORK ACCOMPLISHED ON HAECO N/R 9281113.Jan 28, 2026 · N54241 · Boeing 737824 · Fuselage Main, Longeron/StringerSDR CALA2026012713341Stringer Splice · corrodedAFT CARGO STRINGER SPLICE 22R CORRODED AT BS 887. R & R WITH FABRICATED AFT CARGO STRINGER SPLICE IAW SRM 51-40-02, DWG 146A3250, REV B, & DWG 147A0060, REV A.Jan 24, 2026 · N54241 · Boeing 737824 · Fuselage Main, Longeron/StringerSDR CALA2026012713323Stringer · crackedRIGHT WING INTERNAL FUEL TANK UPPER STRINGER U-9 CRACKED AT THE RIB 21 AREA. ACCOMPLISHED INTERIM REPAIR IAW ECRA 5720-03603 AND REO-G25736.Jan 22, 2026 · N54241 · Boeing 737824 · Wing, Longeron/StringerSDR CALA2026012713320Stringer · crackedLEFT WING INTERNAL FUEL TANK UPPER STRINGER U-9 CRACKED BETWEEN RIB 16 AND RIB 17. ACCOMPLISHED PERMANENT REPAIR IAW ECRA 5720-03602 AND REO-G25734.Jan 21, 2026 · N54241 · Boeing 737824 · Wing, Longeron/StringerSDR CALA2026012213152Rib · wornLEFT OTBD FLAPS NR 1, 2, 3, & 4 AFT FLAP TRACK RIB SUPPORTS HAVE WEAR ON LOWER SURFACES. REMOVED DAMAGE, HFEC AREA, NO DEFECTS NOTED, ROTO PEENED AREA, ALODINED AND PRIMED IAW UAL ECRA 5754-01273, AND ENGINEERING DOC REO-G25762.Jan 20, 2026 · N54241 · Boeing 737824 · Trailing Edge FlapsSDR CALA2026012213148Skin · crackedEA-5720-02922-001 LEFT WING IB LE SKIN HAS 3 FASTENER HOLES WITH CRACK INDICATIONS, HOLE NO. 12, 13, AND 19. ACCOMPLISHED L/E SKIN REPAIR IAW ECRA 5740-03437 AND AAR ENGINEERING DOC REO-25768.Jan 19, 2026 · N54241 · Boeing 737824 · Wing, Plate/SkinSDR CALA2026011612997Shim · migratedVERTICAL STAB LE SIDE INBD REAR SPAR FITTING VSS 1088 HAS A MIGRATING SHIM FROM BETWEEN THE BULKHEAD FITTING AND THE SPAR FITTING. REMOVED MIGRATED LAMINATED SHIMS AND REPLACED WITH SOLID SHIMS IAW DWG 170A1610, REV G, AND IAW AMM 55-30-00.Jan 15, 2026 · N54241 · Boeing 737824 · Vertical Stabilizer, Spar/RibSDR CALA2026020613624Window Frame · crackedFOUND CRACKS AT 3RD AND 4TH LOWER CORNER FASTENER HOLES ON LH SIDE NR 3 WINDOW FRAME CRACKED AT 3RD HOLE IS AT 12 O'CLOCK AND 4TH HOLE IS AT 3 O'CLOCK. REPAIRED THE L3 WINDOW FRAME WITH FREEZE PLUGS, EXTERNAL DOUBLER & TRIPLER, INTERNAL DOUBLER REPAIRS IAW REJan 14, 2026 · N54241 · Boeing 737824 · Fuselage Main, StructureSDR CALA2026011612992Spar · corrodedVERTICAL STAB RT SIDE OTBD REAR SPAR FITTING VSS 1088 HAS A MIGRATING SHIM FROM BETWEEN THE BULKHEAD FITTING AND THE SPAR FITTING. REMOVED MIGRATED LAMINATED SHIM AND REPLACED WITH SOLID SHIMS IAW DWG 170A1610, REV G, AND AMM 55-30-00.Jan 14, 2026 · N54241 · Boeing 737824 · Vertical Stabilizer, Spar/RibSDR CALA2026011612989Skin · damagedAFT CARGO DOOR REQUIRES NEW SKIN, REMOVED AND REPLACED AFT CARGO DOOR OUTER SKIN IAW SRM 52-30-01-2R-3. ALL WORK ACCOMPLISHED ON AAR NR 9280189. REMOVED AND REPLACED OUTER SKIN IAW SRM 52-30-01-2R-3 REP 3, CMM 52-31-14, AND DWG 146A6110 REV C.Jan 12, 2026 · N54241 · Boeing 737824 · Cargo/Baggage DoorsSDR CALA2026011212877Floorbeam · corrodedMAIN CABIN AFT WET AREA, FLOORBEAM HAS CORROSION ON UPPER SURFACE AT BS 986.5 BETWEEN LBL16 AND LBL45. REPAIRED STA 986.5 FLOOR BEAM UPPER SURFACE FROM LBL50 TO RBL50 (FULL T-CAP REPLACEMENT) IAW B737 SRM 53-70-51-2R REPAIR #4 .Jan 8, 2026 · N54241 · Boeing 737824 · Fuselage Main, Floor BeamSDR CALA2026011212876Seat Track · corrodedMAIN CABIN AFT WET AREA, SEAT TRACK HAS CORROSION ON UPPER SURFACE BETWEEN BS907 AND BS927 RBL45. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 REF IPC 53-42-11-34 POST EA. AND IAW NAT DWG 10N00633 REV-.Jan 8, 2026 · N54241 · Boeing 737824 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2026011212875Floorbeam · corrodedMAIN CABIN AFT WET AREA, FLOORBEAM HAS CORROSION ON UPPER SURFACE AT BS 947 APPROX RBL51. REMOVED CORROSIN FROM FLOORBEAM UPPER SURFACE FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A AND UAL ECRA 5321-01330 REV A. REPAIRED DAMAGE IAW SRM 53-70-51-2R, REPAIRJan 8, 2026 · N54241 · Boeing 737824 · Fuselage Main, Floor BeamSDR CALA2026011212874Floorbeam · corrodedB737-53-3-0711 MAIN CABIN AFT WET AREA, FLOOR BEAM HAS CORROSION ON UPPER SURFACE AT BS 947 APPROX LBL51. TRANSCRIBED FROM AAR GSO NRC 9280214. REMOVED EXISTING REPAIR FROM FLOORBEAM, FABRICATED AND INSTALLED REPAIR IAW B737 SRM 53-70-51-2R, REPAIR 5 DETAILJan 8, 2026 · N54241 · Boeing 737824 · Fuselage Main, Floor BeamSDR CALA2026011212873Floor Support · corrodedMAIN CABIN AFT WET AREA, INTERCOSTAL HAS CORROSION ON UPPER SURFACE BETWEEN BS 947.5 AND BS 967 APPROX RBL50. REMOVED CORROSION FROM INTERCOSTAL, UPPER SURFACE, ORIGINAL THICKNESS .125", MATERIAL REMOVED .074", REMAINING MATERIAL .051", FOUND TO BE OUT OF SRMJan 8, 2026 · N54241 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA2026011913048Door Frame · corrodedR2 DOOR CUTOUT AREA, INNER CHORD HAS CORROSION ON UPPER SURFACE BETWEEN BS 927 - 992.8, APPROX. RBL-56. REMOVED CORROSION ON INNER CHORD AT R2 DOOR CUTOUT AREA, UPPER SURFACE BS 927 - BS 992.8, RBL56 ORIGINAL THICKNESS IS .080, REMAINING THICKNESS IS .045 LOSJan 5, 2026 · N54241 · Boeing 737824 · Fuselage Main, StructureSDR CALA2026011913047Door Frame · corrodedL2 DOOR CUTOUT AREA, INNER CHORD HAS CORROSION ON UPPER SURFACE BETWEEN BS 927 TO 992.8 APPROX. LBL-56. REMOVED CORROSION ON INNER CHORD UPPER SURFACE BS 927-992.8 LBL56. ORIGINAL THICKNESS IS .080, REMAINING THICKNESS IS .046, LOSS OF MATERIAL IS .034, FOUNJan 5, 2026 · N54241 · Boeing 737824 · Fuselage Main, StructureSDR CALA2026012213138Stub Beam · gougedR1 DOOR HANDLE BOX CUTOUT, UPPER TORQUE TUBE BUSHING STUB BEAM GOUGED. REMOVED WORN STUB BEAM IAW SRM 51-40-02-0G-0. A NEW STUB BEAM FABRICATED AND INSTALLED IAW SRM 51-40-02 & DWG 141A6516, REV F. RESTORED LEVELING COMPOUND IAW AMM 51-41-11-350-801.Dec 30, 2025 · N54241 · Boeing 737824 · Service DoorsSDR CALA2026010612697Strap · crackedFOUND CRACK INDICATIONS AT LH SIDE STA 616 AFT HOLE OF INBD STUB BEAM STRAP. REMOVED AND REPLACED STRAP ASSY PER BAC DWG # 144A1704 REV: A AND AMM 20-50-11 AND ECRA 5340-02253 REV -Dec 26, 2025 · N54241 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA2026011913044Skin · damagedRIGHT HORIZONTAL STAB LOWER SKIN REQUIRES SKIN CUTOUT AND REPAIR TO FOM AT APPROX STAB STA 92.70. ACCOMPLISHED PERMANENT REPAIR ON RT HORIZONTAL STAB LOWER SKIN BETWEEN HSS 83.50 TO HSS 111.10 IAW SRM 55-10-01-2R-11. THIS IS A CATEGORY 'B' REPAIR AND REQUIREDec 23, 2025 · N54241 · Boeing 737824 · Horizontal Stabilizer, Plate/SkinSDR CALA2026012213134Rib · crackedRIGHT HORIZONTAL STAB INBD SIDE OF RIB AT HSS 101.90 IS CRACKED AT THE LOWER TRANSITION RADIUS OF THE NR 1 VERTICAL STIFFENER. REPAIRED THE NR 1 VERTICAL STIFFENER INBD SIDE OF RIB IAW SRM 55-10-09-2R-4, TABLE 201, REPAIR 4.Dec 19, 2025 · N54241 · Boeing 737824 · Horizontal Stabilizer, Spar/RibSDR CALA2026012213132Rib · crackedRIGHT HORIZONTAL STAB INBD SIDE OF RIB AT HSS 92.70 CRACKED AT THE LOWER TRANSITION RADIUS OF THE NR 4 VERTICAL STIFFENER. REPAIRED NR 4 VERTICAL STIFFENER INBD SIDE OF RIB IAW SRM 55-10-09-2R-4, TABLE 201, REPAIR 4.Dec 19, 2025 · N54241 · Boeing 737824 · Horizontal Stabilizer, Spar/RibSDR CALA2026012213130Rib · crackedRIGHT HORIZIZONAL STAB INBD SIDE OF RIB AT HSS 92.70 IS CRACKED AT THE LOWER TRANSITION RADIUS OF THE NR 3 VERTICAL STIFFENER. REPAIRED THE NR 3 VERTICAL STIFFENER INBD SIDE OF RIB AT HSS 92.70 IAW SRM 55-10-09-2R-4, TABLE 201, REPAIR 4.Dec 19, 2025 · N54241 · Boeing 737824 · Horizontal Stabilizer, Spar/RibSDR CALA2025122412389Rib · crackedRIGHT HORIZONTAL STAB INBD SIDE OF RIB AT HSS 101.90 WAS CRACKED AT THE LOWER TRANSITION RADIUS OF THE NR 2 VERTICAL STIFFENER. REPAIRED NR 2 VERTICAL STIFFENER AND INBD SIDE OF RIB AT STA 101.90 R/H HORIZ STAB IAW B737-800 SRM 55-10-09-2R-4 TABLE 201 REPAIR Dec 19, 2025 · N54241 · Boeing 737824 · Horizontal Stabilizer, Spar/RibSDR CALA2025121812204Floor Support · corrodedMAIN CABIN FLOOR SUPPORT, LBL 44 BETWEEN BS 328 - 344 WAS CORRODED ON UPPER SURFACE JUST IN FRONT OF SEAT TRACK. R & R THE FLOOR SUPPORT IAW DWG 141A5730, REV A.Dec 16, 2025 · N54241 · Boeing 737824 · Fuselage Miscellaneous StructureSDR CALA2025121512086Stringer · crackedFORWARD CARGO STRINGER CLIP AT STA 500I STR26R FWD SIDE IS CRACKED. REMOVED, LOCATED AND DRILLED NEW CLIP STR PN 143A1010-48 PO 1138205.2 & INSTALLED IAW B737 SRM 51-40-05 SRM 51-40-02 BOEING DWG 143A1010 REV A FWD CARGO STRINGER CLIP STA 500I STR 26R.Dec 10, 2025 · N54241 · Boeing 737824 · Fuselage Main, Longeron/StringerSDR CALA2025092909362Girt Bar · no discrepancyDOOR 2L SLIDE GIRT BAR HAS EXCESS SLIDE MATERIAL MEASURED GIRT. OK PER MM25-66-01.Sep 26, 2025 · N54241 · Boeing 737824 · Emergency EquipmentSDR CALA2025082007957Collar · failed2L RIGHT GIRTH BAR COLAR IS COMING APART. RESECURED GIRT BAR COLLAR COVER, OPS CHECKS ARE GOOD. ACFT GOOD TO CONTINUE.Aug 16, 2025 · N54241 · Boeing 737824 · Emergency EquipmentSDR CALA2025081807870Battery Pack · inoperativeFORWARD PAX ENTRY DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. RELAMPED FORWARD PAX DOOR EXTIRIOR LIGHT IAW AMM 33-51-04-960-801. NO HELP. NOTED EXIT SIGH FOR THE DOOR IS OUT. CHANGED BATTERY CHARGER FOR ASSOCIATED SECTION IAW AMM 33-51-06-960-806. NO HELP. SEAug 15, 2025 · N54241 · Boeing 737824 · Emergency LightingSDR CALA2025070706309Hub Cap · missingNR 2 MLG TIRE MISSING HUB CAP INSTALLED NEW HUBCAP ON #2 MLG TIRE REF AMM 32-45-11-400-801.Jul 3, 2025 · N54241 · Boeing 737824 · Wheel/Ski/FloatSDR CALA2025062705982Slide · exposedFA REPORTS DOOR 1R SLIDE MATERIAL HANGING ON FLOOR INSPECTED R1 DOOR ESCAPE SLIDE SYS, RESECURED GIRT MATERIAL INTO SLIDE COVER. GIRT MATERIAL SHOWING WITHIN SERVICEABLE LIMITS REF AMM 25-66-01-400-803. OK TO CONTINUE SERVICE.Jun 26, 2025 · N54241 · Boeing 737824 · Escape SlideSDR CALA2024092000663Autothrottle Sys · faultedTOGA WOULD NOT ENGAGE WHEN SETTING TAKEOFF THRUST AUTOTHROTTLE TOGA OPS CK REF AMM 22-32-TASK 804 TEST PASSSep 15, 2024 · N54241 · Boeing 737824 · Auto Throttle SystemSDR CALA2024091600633Skin · crackedLH WING - OUTBOARD LOWER WING SKIN - IS CRACKED AT FASTENER - LOCTED AT STRINGER S-9L - BETWEEN WSTA 56405 - 591.5. DIP IS NOT RII REF GMM 09-25-05 DIP IS NOT RII REF GMM 09-25-05 DIP IS NOT RII REF GMM 09-25-05 IAW ECRA# 5725-01141 ITEM E (1). ON LEFT WING LOSep 13, 2024 · N54241 · Boeing 737824 · Wing, Plate/SkinSDR CALA2023041701148Seal · missingPDA 1 SEAL SECTION MISSING. LFT WING. #3 TRAILING EDGE FLAP FAIRING OTBD SIDE. REF IPC27-51-18-03. ITEM #160. PN 5750DA15290-1. M&E 29-2751-3-0616. ITERIM REPAIR MADE PER ECRA 2751-01732 PART 1. INTERIM REPAIR PER PART 1 OF ECRA 2751-01873. ADD EMP:U027754 ADDApr 17, 2023 · N54241 · Boeing 7378 · Flight Control SystemSDR CALA2022090502273Nozzle · missingPDA 3 #1 ENG PRIMARY EXHAUST NOZZLE INBOARD SIDE FWD FENCE HAS ELONGATED HOLE AND MISSING FASTENER (SECOND FROM AFT). REMOVED #1 ENG EXHAUST NUZZLE. REMOVED AND REPLACED #1ENG PRIMARY NOZZLE.Sep 5, 2022 · N54241 · Boeing 737 · Engine Exhaust SystemSDR CALA2022032100739Service Door · missingPDA 1 LAVATORY SERVICE DOOR FOUND MISSING UPON ARRIVAL IN BNA AFTER FLIGHT UA771 (DEN / BNA). DOOR (145AL)MEASURES IN EXCESS OF 150 SQ INCHES AND WILL BE DESIGNATED A CATEGORY 1. SDR #1028039 SUBMITTED AS PER GMM 02-30-95 AND ESC HAS BEEN ADVISED. SDR #1028039Mar 21, 2022 · N54241 · Boeing 737800* · Service DoorsSDR CALA2022032100711Service Door · missingLAV SERVICE PANEL ON AFT FUSELAGE MISSING. CONFIRMED LAVATORY SERVICE DOOR IS MISSING. PERFORMED A ENHANCED ZONAL INSPECTION OF THE AFT LOWER FUSELAGE AND EMPENNAGE AREA IN REFERENCE WITH 05-42-01-210-801. NO DAMAGED NOTED. PLACING DOOR ON CDL IN REFERENCE WIMar 18, 2022 · N54241 · Boeing 737800* · DoorsSDR CALA2022030700575Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRACKED. SUPPORT TASK NSA EMX NR 00091. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 RBL 54.60 IAW B737-800 SRM 51-40-02 AND DWG 111A2000 REV ORG. DATA WAS TRA NSCRIIBED FROM EMX 00091 WORK Mar 4, 2022 · N54241 · Boeing 737800* · Wing StructureSDR CALA2022030700574Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 40.87 IS CRACKED. SUPPORT TASK NSA EMX NR 00090. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 RBL 40.87. 3/4/22 IAW B737-800 SRM 51-40-02 AND DWG 111A2000 REV ORIGINAL. DATA W AS TRANSCRIBED FROM NSMar 4, 2022 · N54241 · Boeing 737800* · Wing StructureSDR CALA2022030700573Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX NR 00089. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 RBL 32.40 2 IAW B737-800 SRM 51-40-02 AND DWG 111A2000 REV. ORIGINAL DATA WA S TRANSCRIBED FROM EMX 00089Mar 4, 2022 · N54241 · Boeing 737800* · Wing StructureSDR CALA2022030700572Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX NR 00088. REMOVED AND REPLACED CRACKED SHEAR FITTING AT SA 540 RBL 15.04 I SSFR REPORT FORM 46-0024 ENTERED BY UAL INSPECTION U354653 AW B737-800 SRM 51-40-02 AND DWG 11Mar 4, 2022 · N54241 · Boeing 737800* · Wing StructureSDR CALA2022030700571Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED. SUPPORT TASK NSA EMX NR 00087. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 RBL 6.14 I INSPECTION U354653 ON 03/04/22 AW B737-800 SRM 51-40-02 AND DWG 111A2000 REV ORG. DATA WAS TRAMar 4, 2022 · N54241 · Boeing 737800* · Wing StructureSDR CALA2022030700570Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 54.60 IS CRACKED. SUPPORT TASK NSA EMX NR 00086. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 LBL 54.60 U354653 ON 03/04/22 IAW B737-800 SRM 51-40-02 AND DWG 111A2000 REV ORG. DATA WAS TRA NSCRIBED FMar 4, 2022 · N54241 · Boeing 737800* · Wing StructureSDR CALA2022030700569Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 40.87 IS CRACKED. SUPPORT TASK NSA EMX NR 00085. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 LBL 40.87 ECTION U354653 ON 03/04/22 IAW B737-800 SRM 51-40-02 AND DWG 111A2000 REV ORG DATA WAS TRAN SCRMar 4, 2022 · N54241 · Boeing 737800* · Wing StructureSDR CALA2022030700568Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX NR 00084. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 LBL 32.40 U354653 ON 03/04/22 B737-800 SRM 51-40-02 AND DWG 111A2000 REV ORG. DATA WAS TRANSCR IBED FROM Mar 4, 2022 · N54241 · Boeing 737800* · Wing StructureSDR CALA2022030700567Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX NR 00083. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540 LBL 15.04 U354653 ON 03/04/22 IAW B737-800 SRM 51-40-02 AND DWG 111A2000 REV ORG. DATA WAS TRA NSCRIBED FMar 4, 2022 · N54241 · Boeing 737800* · Wing StructureSDR CALA2022030700566Fitting · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 6114 IS CRACKED. SUPPORT TASK NSA EMX NR 00082. REMOVED AND REPLACED CRACKED SHEAR FITTING AT STA 540LBL 6.14 IA ION U354653 ON 03/04/22 W B737-800 SRM 51-40-02 AND DWG 111A2000 REV ORG. DATA WAS TRAN SCIBEDMar 4, 2022 · N54241 · Boeing 737800* · Wing StructureSDR CALA2018022100725Light · brokenSEAT ROW 15C EMERGENCY EXIT LIGHT BROKEN FROM SEAT. REPLACED THE LIGHT ASSEMBLY, OPS CHECKED GOOD. MM 33-51-00. ACCOMPLISHED IDT INSPECTION IAW GMM 09-10-05 & AMM 33-51-00. NO DEFECTS NOTED.Feb 21, 2018 · N54241 · Boeing 737824 · Emergency LightingSDR CALA2018021600656Light · inoperativeSEAT 15C EMERGENCY EXIT LIGHT NOT WORKING. THE EMERGENCY LIGHT WAS REPLACED.Feb 16, 2018 · N54241 · Boeing 737824 · Emergency LightingSDR CALA2017120204291Eec · faultyON CLIMB ENG 2 WOULDNT GO TO CLB THRUST. AT 10000 ENG1-97.1ENG 2-95.9 15000 ENG1-96.0ENG2-93.7 EEC BITE TEST #2 ENG RESCENT FAULTS: ALTERNATOR VOLTAGE MSG NBR: 73-21282 AND GROUND TEST INTERNAL EEC FAULT MSG NBR: 73-20102. PER FIM 73-27-00-810-805-F00 AND 73Dec 2, 2017 · N54241 · Boeing 737824 · Fuel Controlling System
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