# Service difficulty reports: Boeing 737-48E A list on [Boeing 737-48E](https://openairdocs.org/model/boeing-737-48e.md). Newest first. General aviation reporting is voluntary. Page 1 of 4 · 189 reports - [SDR I5EA2023101400001](https://openairdocs.org/sdr/I5EA2023101400001.md): Unknown · unknown · Oct 14, 2023 · N545CC · Boeing 73748E · Fuselage Main, Plate/Skin > CRACK ON FUSELAGE STA 727+6 STR 10R. REPAIRED FUSELAGE SKIN AT STA 727+6 STR 10R IAW BOEING MESSAGE SFW-SFW 23-0162-07B. - [SDR I5EA2023091600007](https://openairdocs.org/sdr/I5EA2023091600007.md): Battery Pack · no test · Sep 16, 2023 · N545CC · Boeing 73748E · Emergency Lighting > MODULE M1673 POWER SUPPLY BAD. REMOVED AND REPLACED M1673 POWER SUPPLY AT STA 973 IAW B737-400 AMM 33-51-51. TEST OK. - [SDR I5EA2023091600006](https://openairdocs.org/sdr/I5EA2023091600006.md): Battery Pack · no test · Sep 16, 2023 · N545CC · Boeing 73748E · Emergency Lighting > AFT ENTRY DOOR EXIT IDENTIFIER FOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M1673 AT STA 973 WITH SERVICEABLE UNIT AND TEST IAW B737-400 AMM 33-51-51. TEST OK. - [SDR I5EA2023033000001](https://openairdocs.org/sdr/I5EA2023033000001.md): Battery Pack · inoperative · Mar 30, 2023 · N545CC · Boeing 73748E · Emergency Lighting > FWD RIGHT EMERGENCY ESCAPE SLIDE LIGHT INOP - REMOVED AND REPLACED BATTERY PACK M1674 STA 324 WL 293 BL R7 IAW B737-400 AMM 33-51-51 - [SDR I5EA2022111100005](https://openairdocs.org/sdr/I5EA2022111100005.md): Battery Pack · inoperative · Nov 10, 2022 · N545CC · Boeing 73748E · Emergency Lighting > LEFT EMERGENCY EXIT LIGHT A/C LATCH INOP (LP 101907). REMOVED AND REPALCED BATTERY PACK LH MID IAW B737 AMM 33-51-51, OPAS CHECK GOOD - [SDR I5EA2021081200010](https://openairdocs.org/sdr/I5EA2021081200010.md): Battery Pack · discharged · Aug 11, 2021 · N538CC · Boeing 73748E · Emergency Lighting > CABIN BATTERT PACK LIGHT IS INOP CONNECTOR ( MO1672). REMOVED AND REPLACED THE BATTERY PACK EMERGENCY LIGHT CONNECTOR M01672. OPS CHECK TEST OK. IAW B737 AMM 33-51-51. - [SDR I5EA2020011402](https://openairdocs.org/sdr/I5EA2020011402.md): Light · inoperative · Jan 8, 2020 · N545CC · Boeing 73748E · Emergency Lighting > EMERGENCY LIGHT INOP AT M1695, STA565, WL213, RBL68 - [SDR I5EA2019121707](https://openairdocs.org/sdr/I5EA2019121707.md): Gcu · malfunctioned · Dec 15, 2019 · N538CC · Boeing 73748E · AC Generator-Alternator > #1 ENGINE GENERATOR WENT OFF LINE. APU ALREADY ON MEL. SYSTEM "B" HYD PRESS LOW LIGHT, YAW DAMP OFF, EQUIPMENT COOLING FAN OFF, ANTI-SKID INOP, MULTIPLE LOW PRESSURE LIGHTS. - [SDR I5EA2019012202](https://openairdocs.org/sdr/I5EA2019012202.md): Oxygen Gen · unwanted deploy · Jan 21, 2019 · N538CC · Boeing 73748E · Passenger Oxygen System > DISCREPANCY: 1/21/2019, LP 29887 - ROW 24DEF OXYGEN GENERATOR INADVERTENTLY DEPLOYED DURING MAINTENANCE INSPECTION. CORRECTIVE ACTION: 1/25/2019, LP 29888 - REMOVED AND REPLACED OXYGEN GENERATOR IAW AMM 35-22-11. - [SDR I5EA201812030001](https://openairdocs.org/sdr/I5EA201812030001.md): Fan · inoperative · Dec 1, 2018 · N538CC · Boeing 73748E · Air Distribution Fan > DISCREPANCY: L/P 27388 - ITEM 1 - 30 MINUTES OUTSIDE OF MEM, THE LEAD FA INFORMED THE FLT DECK OF FUMES IN THE CABIN, DESCRIBED AS AN ELECTRICAL BURN SMELL, WITH THE FLIGHT DECK DOOR OPENED, IT COULD BE SMELLED ON THE FLIGHT DECK. RAN THE "SMOKE, FIRE, FUMES" - [SDR I5EA201811300004](https://openairdocs.org/sdr/I5EA201811300004.md): Unknown · odor · Nov 29, 2018 · N538CC · Boeing 73748E · Air Distribution System > DISCREPANCY: L/P 27385 - AT 34,000' THE CABIN CREW CALLED THE FLIGHT DECK TO INFORM THE PILOTS THEY SMELLED SMOKE IN THE CABIN. WHEN THEY OPENED THE FLIGHT DECK DOOR THE PILOTS COULD SMELL A STRONG ODOR OF SMOKE. THEY DONNED THEIR OXYGEN MASKS AND REQUESTED - [SDR I5EA2018102209](https://openairdocs.org/sdr/I5EA2018102209.md): Indicator · malfunctioned · Oct 21, 2018 · N538CC · Boeing 73748E · Trailing Flap Position Indicating System > DISCREPANCY: FLAPS EXTENDED TO 10 UNITS WITH FLAP HANDLE, GREATER THAN 1 UNITS, FLAP DISAGREEMENT CONDITION. CORRECTIVE ACTION: PERFORMED GENERAL VISUAL INSPECTION OF FLAP DRIVE SYS. AND ASSOCIATED COMPONENTS. NO FAULTS NOTED IAW AMM 27-58-41. REMOVED AND - [SDR I5EA2018101004](https://openairdocs.org/sdr/I5EA2018101004.md): Slide · unwanted deploy · Oct 9, 2018 · N545CC · Boeing 73748E · Escape Slide > DISCREPANCY: R1 DOOR SLIDE DEPLOYED DURING REPACK. CORRECTIVE ACTION: REMOVED AND INSTALLED EMERGENCY DOOR SLIDE IAW AMM 25-61-35 AT R1 DOOR. - [SDR FOTR20180814007](https://openairdocs.org/sdr/FOTR20180814007.md): Bushing · corroded · Aug 14, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Structure > RT STAB FORWARD LOWER SPAR JOINT LUG HAS CORROSION ON FWD. FACE - [SDR FOTR20180814006](https://openairdocs.org/sdr/FOTR20180814006.md): Bushing · corroded · Aug 14, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Structure > RH STAB. FWD. SPAR FITTING LOWER CLEVIS AFT FACE HAS CORROSION (AIRCRAFT SIDE) - [SDR FOTR20180814005](https://openairdocs.org/sdr/FOTR20180814005.md): Bushing · corroded · Aug 14, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Structure > RIGHT STAB FORWARD SPAR FITTING LOWER, FWD, CLEVIS, FWD FACE HAD CORROSION (AIRCRAFT SIDE) - [SDR FOTR20180814004](https://openairdocs.org/sdr/FOTR20180814004.md): Bushing · corroded · Aug 14, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Structure > RIGHT STAB FORWARD SPAR FITTING AFT, UPPER CLEVIS-AFT FACE HAS CORROSION (AIRCRAFT SIDE). - [SDR FOTR20180814003](https://openairdocs.org/sdr/FOTR20180814003.md): Bushing · corroded · Aug 14, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Structure > RIGHT STAB FORWARD SPAR FITTING UPPER FWD. CLEVIS FACE HAS CORROSION (AIRCRAFT SIDE) - [SDR FOTR20180814002](https://openairdocs.org/sdr/FOTR20180814002.md): Bushing · corroded · Aug 14, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Structure > RH STABILIZER, FORWARD UPPER SPAR JOINT LUG HAS CORROSION ON FWD. FACE OF BUSHING - [SDR FOTR20180814001](https://openairdocs.org/sdr/FOTR20180814001.md): Bushing · corroded · Aug 14, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Structure > LEFT HORIZONTAL STABILIZER FWD ATTACH LUG, UPPER BUSHING, HAD CORROSION. - [SDR 2019F00051](https://openairdocs.org/sdr/2019F00051.md): Bushing · corroded · Aug 14, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Structure > LEFT STABILIZER, CENTER SECTION FRONT SPAR UPPER AFT CLEVIS, HAS CORROSION (AIRCRAFT SIDE) - [SDR 2019F00050](https://openairdocs.org/sdr/2019F00050.md): Bushing · corroded · Aug 14, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Structure > LEFT STAB. CENTER SECTION FRONT SPAR UPPER FWD CLEVIS HAS CORROSION (AIRCRAFT SIDE) - [SDR 2019F00049](https://openairdocs.org/sdr/2019F00049.md): Bushing · corroded · Aug 14, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Structure > LEFT HORIZONTAL STABILIZER, FWD. ATTACH LUG, LOWER BUSHING HAS CORROSION (STABILIZER SIDE) - [SDR 2019F00048](https://openairdocs.org/sdr/2019F00048.md): Bushing · corroded · Aug 14, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Structure > LH STAB. FORWARD SPAR FITTING, FWD FACE OF LOWER CLEVIS, HAS CORROSION (AIRCRAFT SIDE) - [SDR 2019F00047](https://openairdocs.org/sdr/2019F00047.md): Bushing · corroded · Aug 14, 2018 · N480VX · Boeing 73748E · Empennage Structure > LEFT LOWER AFT, FWD. STAB CLEVIS HAS CORROSION AROUND BUSHING - [SDR 2019F00046](https://openairdocs.org/sdr/2019F00046.md): Skin · cracked · Aug 14, 2018 · N480VX · Boeing 73748E · Wing, Plate/Skin > .5 INCH CRACK LOCATED THROUGH FASTENER UPPER LT WING SKIN AT WS 259, INBD. OF PYLON, 4 INCHES AWAY FROM TRIPLER. - [SDR FOTR2018080700334](https://openairdocs.org/sdr/FOTR2018080700334.md): Skin · damaged · Aug 7, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer, Plate/Skin > RIGHT HORIZONTAL STAB, REMOVABLE L/E OTBD. END HAS ELONGATED HOLE. - [SDR 2018FA0000312](https://openairdocs.org/sdr/2018FA0000312.md): Lug · corroded · Jul 31, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Miscellaneous Structure > RT STAB AFT UPPER SPAR JOINT LUG HAS CORROSION ON FWD FACE. - [SDR 2018FA0000311](https://openairdocs.org/sdr/2018FA0000311.md): Clevis · corroded · Jul 31, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Miscellaneous Structure > RT STAB AFT SPAR FITTING AFT UPPER CLEVIS AFT FACE HAS CORROSION ( AIRCRAFT SIDE). - [SDR 2018FA0000310](https://openairdocs.org/sdr/2018FA0000310.md): Clevis · corroded · Jul 31, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Miscellaneous Structure > RT STAB AFT SPAR FITTING FWD UPPER CLEVIS FWD FACE HAS CORROSION (AIRCRAFT SIDE). - [SDR 2018FA0000309](https://openairdocs.org/sdr/2018FA0000309.md): Clevis · corroded · Jul 31, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Miscellaneous Structure > LT STAB REAR SPAR FWD FAIL SAFE CLEVIS HAS CORROSION. - [SDR 2018FA0000308](https://openairdocs.org/sdr/2018FA0000308.md): Clevis · corroded · Jul 31, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Miscellaneous Structure > LT STABILIZER REAR SPAR AFT FAILSAFE CLEVIS HAS CORROSION (AFT SPAR) AT 7591. - [SDR 2018FA0000307](https://openairdocs.org/sdr/2018FA0000307.md): Lug · corroded · Jul 31, 2018 · N480VX · Boeing 73748E · Horizontal Stabilizer Miscellaneous Structure > LT HORIZONTAL STABILIZER AFT ATTACH LUG CENTER BUSHING AFT FACE HAS CORROSION (STABILIZER SIDE). - [SDR FOTR201806220001](https://openairdocs.org/sdr/FOTR201806220001.md): Floorbeam · corroded · Jun 22, 2018 · N480VX · Boeing 73748E · Fuselage Main, Floor Beam > MAIN CABIN BS 340, STRINGERS 17L - 17R, FLOORBEAM CORRODED, TOP SIDE. - [SDR FOTR201806190001](https://openairdocs.org/sdr/FOTR201806190001.md): Floorbeam · corroded · Jun 19, 2018 · N480VX · Boeing 73748E · Fuselage Main, Floor Beam > CORROSION ON PASSENGER CABIN FLOORBEAM BS 947.5, THE ENTIRE LENGTH - [SDR FOTR201805310001](https://openairdocs.org/sdr/FOTR201805310001.md): Floor Support · cracked · May 31, 2018 · N480VX · Boeing 73748E · Fuselage Miscellaneous Structure > FLOOR SUPPORT, BS 344 - 360, LBL 26 HAD A 3/8 INCH CRACK IN THE LOWER FLANGE. - [SDR FOTR20180515004](https://openairdocs.org/sdr/FOTR20180515004.md): Floorbeam · corroded · May 15, 2018 · N480VX · Boeing 73748E · Fuselage Main, Floor Beam > CORROSION ON THE PASSENGER CABIN FLOORBEAM BS 986.5, ENTIRE LENGTH - [SDR FOTR20180515003](https://openairdocs.org/sdr/FOTR20180515003.md): Frame · cracked · May 15, 2018 · N480VX · Boeing 73748E · Fuselage Main, Frame > RIGHT BS 360 FRAME IS CRACKED AT THE INBD FASTENER HOLE OF THE AIR CONDITIONING ATTACH BRACKET FOR STRINGER 8R. - [SDR FOTR20180515002](https://openairdocs.org/sdr/FOTR20180515002.md): Threshold · corroded · May 15, 2018 · N480VX · Boeing 73748E · Fuselage Miscellaneous Structure > R2 SERVICE DOOR BOTTOM INNER THRESHOLD CUTOUT ON FUSELAGE UPPER SURFACE FOUND CORRODED 30 SQUARE INCHES FROM BS 947 TO 1011.5. - [SDR FOTR20180515001](https://openairdocs.org/sdr/FOTR20180515001.md): Threshold · corroded · May 15, 2018 · N480VX · Boeing 73748E · Fuselage Miscellaneous Structure > L2 DOOR THRESHOLD CUTOUT ON FUSELAGE, UPPER SURFACE CORRODED 15 SQUARE INCHES. - [SDR FOTR20180501001](https://openairdocs.org/sdr/FOTR20180501001.md): Web · corroded · May 1, 2018 · N480VX · Boeing 73748E · Fuselage Miscellaneous Structure > MAIN CABIN BETWEEN BS 332 - 348, STRINGER 12R CORROSION ON WEB. - [SDR FOTR20180425004](https://openairdocs.org/sdr/FOTR20180425004.md): Floorbeam · corroded · Apr 25, 2018 · N480VX · Boeing 73748E · Fuselage Main, Floor Beam > MAIN CABIN FLOORBEAM BS 967 UPPER FLANGE, UPPER SURFACE FOUND CORRODED 5 SQUARE INHCES, LBL 18, 30, 42, AND 48. - [SDR FOTR20180425003](https://openairdocs.org/sdr/FOTR20180425003.md): Door Frame · gouged · Apr 25, 2018 · N480VX · Boeing 73748E · Fuselage Main, Structure > AFT CARGO DOOR FWD FRAME HAS A.50 INCH GOUGE AT STRINGER 24 AND.50 INCH GOUGE 4 INCHES BELOW. - [SDR FOTR20180425002](https://openairdocs.org/sdr/FOTR20180425002.md): Floor Support · corroded · Apr 25, 2018 · N480VX · Boeing 73748E · Fuselage Miscellaneous Structure > CORROSION ON THE AFT CARGO COMPARTMENT FLOOR SUPPORT, INBD SURFACE AND AROUND FASTENER HOLE. - [SDR FOTR20180425001](https://openairdocs.org/sdr/FOTR20180425001.md): Web · corroded · Apr 25, 2018 · N480VX · Boeing 73748E · Fuselage Miscellaneous Structure > CORROSION ON THE AFT CARGO COMPARTMENT WEB BETWEEN BS 787 AND 794, RBL. 19.5. - [SDR FOTR20180421003](https://openairdocs.org/sdr/FOTR20180421003.md): Web · corroded · Apr 21, 2018 · N480VX · Boeing 73748E · Fuselage Miscellaneous Structure > CORROSION IN THE AFT CARGO BAY WEB BETWEEN BS 795 AND 820, RBL 19.5. - [SDR FOTR20180421002](https://openairdocs.org/sdr/FOTR20180421002.md): Angle · corroded · Apr 21, 2018 · N480VX · Boeing 73748E · Fuselage Miscellaneous Structure > AFT CARGO BAY FLOOR SUPPORT BS 787 TO 794, RBL 20 IN FILLER STRIP CORRODED 10 SQ. INCHES. - [SDR FOTR20180421001](https://openairdocs.org/sdr/FOTR20180421001.md): Floorbeam · corroded · Apr 21, 2018 · N480VX · Boeing 73748E · Fuselage Main, Floor Beam > CORROSION AROUND FASTENER HOLES ON THE AFT CARGO BAY FLOORBEAM, FWD ATTACH ANGLE BS 795 BETWEEN STRINGERS 25R AND 26R. - [SDR FOTR20180413001](https://openairdocs.org/sdr/FOTR20180413001.md): Attach Bracket · corroded · Apr 13, 2018 · N480VX · Boeing 73748E · Fuselage Miscellaneous Structure > CABIN L-2 ENTRANCE DOOR INNER LWR CUTOUT AT STA 993.5 VERT ATTACH BRKT AT FLOOR LEVEL CORRODED 5 SQ IN. - [SDR FOTR20180411004](https://openairdocs.org/sdr/FOTR20180411004.md): Floor Support · cracked · Apr 11, 2018 · N480VX · Boeing 73748E · Fuselage Miscellaneous Structure > FLOOR SUPPORT AT BS 344 - 360, RBL 32 HAS 1/2 INCH CRACK. Next page: https://openairdocs.org/model/boeing-737-48e/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 aircraft_model_key = '73748E' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/boeing-737-48e/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.