# Service difficulty reports: N54241

A list on [N54241](https://openairdocs.org/aircraft/N54241.md).

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

Page 1 of 3 · 117 reports

- [SDR CALA2026012913425](https://openairdocs.org/sdr/CALA2026012913425.md): Stringer · corroded · Jan 28, 2026 · N54241 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > AFT CARGO AREA, FOUND ADDITIONAL CORROSION ON STRINGER 22R, BS 887. MAJOR REPAIR. DIP LPS 7747663 & 7747714. WORK ACCOMPLISHED ON HAECO N/R 9281113.
- [SDR CALA2026012713341](https://openairdocs.org/sdr/CALA2026012713341.md): Stringer Splice · corroded · Jan 24, 2026 · N54241 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > AFT 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.
- [SDR CALA2026012713323](https://openairdocs.org/sdr/CALA2026012713323.md): Stringer · cracked · Jan 22, 2026 · N54241 · Boeing 737824 · Wing, Longeron/Stringer
  > RIGHT WING INTERNAL FUEL TANK UPPER STRINGER U-9 CRACKED AT THE RIB 21 AREA. ACCOMPLISHED INTERIM REPAIR IAW ECRA 5720-03603 AND REO-G25736.
- [SDR CALA2026012713320](https://openairdocs.org/sdr/CALA2026012713320.md): Stringer · cracked · Jan 21, 2026 · N54241 · Boeing 737824 · Wing, Longeron/Stringer
  > LEFT 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.
- [SDR CALA2026012213152](https://openairdocs.org/sdr/CALA2026012213152.md): Rib · worn · Jan 20, 2026 · N54241 · Boeing 737824 · Trailing Edge Flaps
  > LEFT 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.
- [SDR CALA2026012213148](https://openairdocs.org/sdr/CALA2026012213148.md): Skin · cracked · Jan 19, 2026 · N54241 · Boeing 737824 · Wing, Plate/Skin
  > EA-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.
- [SDR CALA2026011612997](https://openairdocs.org/sdr/CALA2026011612997.md): Shim · migrated · Jan 15, 2026 · N54241 · Boeing 737824 · Vertical Stabilizer, Spar/Rib
  > VERTICAL 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.
- [SDR CALA2026020613624](https://openairdocs.org/sdr/CALA2026020613624.md): Window Frame · cracked · Jan 14, 2026 · N54241 · Boeing 737824 · Fuselage Main, Structure
  > FOUND 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 RE
- [SDR CALA2026011612992](https://openairdocs.org/sdr/CALA2026011612992.md): Spar · corroded · Jan 14, 2026 · N54241 · Boeing 737824 · Vertical Stabilizer, Spar/Rib
  > VERTICAL 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.
- [SDR CALA2026011612989](https://openairdocs.org/sdr/CALA2026011612989.md): Skin · damaged · Jan 12, 2026 · N54241 · Boeing 737824 · Cargo/Baggage Doors
  > AFT 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.
- [SDR CALA2026011212877](https://openairdocs.org/sdr/CALA2026011212877.md): Floorbeam · corroded · Jan 8, 2026 · N54241 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN 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.
- [SDR CALA2026011212876](https://openairdocs.org/sdr/CALA2026011212876.md): Seat Track · corroded · Jan 8, 2026 · N54241 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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-.
- [SDR CALA2026011212875](https://openairdocs.org/sdr/CALA2026011212875.md): Floorbeam · corroded · Jan 8, 2026 · N54241 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN 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, REPAIR
- [SDR CALA2026011212874](https://openairdocs.org/sdr/CALA2026011212874.md): Floorbeam · corroded · Jan 8, 2026 · N54241 · Boeing 737824 · Fuselage Main, Floor Beam
  > B737-53-3-0711 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 DETAIL
- [SDR CALA2026011212873](https://openairdocs.org/sdr/CALA2026011212873.md): Floor Support · corroded · Jan 8, 2026 · N54241 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN 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 SRM
- [SDR CALA2026011913048](https://openairdocs.org/sdr/CALA2026011913048.md): Door Frame · corroded · Jan 5, 2026 · N54241 · Boeing 737824 · Fuselage Main, Structure
  > R2 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 LOS
- [SDR CALA2026011913047](https://openairdocs.org/sdr/CALA2026011913047.md): Door Frame · corroded · Jan 5, 2026 · N54241 · Boeing 737824 · Fuselage Main, Structure
  > L2 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, FOUN
- [SDR CALA2026012213138](https://openairdocs.org/sdr/CALA2026012213138.md): Stub Beam · gouged · Dec 30, 2025 · N54241 · Boeing 737824 · Service Doors
  > R1 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.
- [SDR CALA2026010612697](https://openairdocs.org/sdr/CALA2026010612697.md): Strap · cracked · Dec 26, 2025 · N54241 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FOUND 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 -
- [SDR CALA2026011913044](https://openairdocs.org/sdr/CALA2026011913044.md): Skin · damaged · Dec 23, 2025 · N54241 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RIGHT 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 REQUIRE
- [SDR CALA2026012213134](https://openairdocs.org/sdr/CALA2026012213134.md): Rib · cracked · Dec 19, 2025 · N54241 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > RIGHT 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.
- [SDR CALA2026012213132](https://openairdocs.org/sdr/CALA2026012213132.md): Rib · cracked · Dec 19, 2025 · N54241 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > RIGHT 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.
- [SDR CALA2026012213130](https://openairdocs.org/sdr/CALA2026012213130.md): Rib · cracked · Dec 19, 2025 · N54241 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > RIGHT 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.
- [SDR CALA2025122412389](https://openairdocs.org/sdr/CALA2025122412389.md): Rib · cracked · Dec 19, 2025 · N54241 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > RIGHT 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
- [SDR CALA2025121812204](https://openairdocs.org/sdr/CALA2025121812204.md): Floor Support · corroded · Dec 16, 2025 · N54241 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR CALA2025121512086](https://openairdocs.org/sdr/CALA2025121512086.md): Stringer · cracked · Dec 10, 2025 · N54241 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > FORWARD 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.
- [SDR CALA2025092909362](https://openairdocs.org/sdr/CALA2025092909362.md): Girt Bar · no discrepancy · Sep 26, 2025 · N54241 · Boeing 737824 · Emergency Equipment
  > DOOR 2L SLIDE GIRT BAR HAS EXCESS SLIDE MATERIAL MEASURED GIRT. OK PER MM25-66-01.
- [SDR CALA2025082007957](https://openairdocs.org/sdr/CALA2025082007957.md): Collar · failed · Aug 16, 2025 · N54241 · Boeing 737824 · Emergency Equipment
  > 2L RIGHT GIRTH BAR COLAR IS COMING APART. RESECURED GIRT BAR COLLAR COVER, OPS CHECKS ARE GOOD. ACFT GOOD TO CONTINUE.
- [SDR CALA2025081807870](https://openairdocs.org/sdr/CALA2025081807870.md): Battery Pack · inoperative · Aug 15, 2025 · N54241 · Boeing 737824 · Emergency Lighting
  > FORWARD 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. SE
- [SDR CALA2025070706309](https://openairdocs.org/sdr/CALA2025070706309.md): Hub Cap · missing · Jul 3, 2025 · N54241 · Boeing 737824 · Wheel/Ski/Float
  > NR 2 MLG TIRE MISSING HUB CAP INSTALLED NEW HUBCAP ON #2 MLG TIRE REF AMM 32-45-11-400-801.
- [SDR CALA2025062705982](https://openairdocs.org/sdr/CALA2025062705982.md): Slide · exposed · Jun 26, 2025 · N54241 · Boeing 737824 · Escape Slide
  > FA 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.
- [SDR CALA2024092000663](https://openairdocs.org/sdr/CALA2024092000663.md): Autothrottle Sys · faulted · Sep 15, 2024 · N54241 · Boeing 737824 · Auto Throttle System
  > TOGA WOULD NOT ENGAGE WHEN SETTING TAKEOFF THRUST AUTOTHROTTLE TOGA OPS CK REF AMM 22-32-TASK 804 TEST PASS
- [SDR CALA2024091600633](https://openairdocs.org/sdr/CALA2024091600633.md): Skin · cracked · Sep 13, 2024 · N54241 · Boeing 737824 · Wing, Plate/Skin
  > LH 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 LO
- [SDR CALA2023041701148](https://openairdocs.org/sdr/CALA2023041701148.md): Seal · missing · Apr 17, 2023 · N54241 · Boeing 7378 · Flight Control System
  > PDA 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 ADD
- [SDR CALA2022090502273](https://openairdocs.org/sdr/CALA2022090502273.md): Nozzle · missing · Sep 5, 2022 · N54241 · Boeing 737 · Engine Exhaust System
  > PDA 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.
- [SDR CALA2022032100739](https://openairdocs.org/sdr/CALA2022032100739.md): Service Door · missing · Mar 21, 2022 · N54241 · Boeing 737800* · Service Doors
  > PDA 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 #1028039
- [SDR CALA2022032100711](https://openairdocs.org/sdr/CALA2022032100711.md): Service Door · missing · Mar 18, 2022 · N54241 · Boeing 737800* · Doors
  > LAV 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 WI
- [SDR CALA2022030700575](https://openairdocs.org/sdr/CALA2022030700575.md): Fitting · cracked · Mar 4, 2022 · N54241 · Boeing 737800* · Wing Structure
  > B737-57-4-1262-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
- [SDR CALA2022030700574](https://openairdocs.org/sdr/CALA2022030700574.md): Fitting · cracked · Mar 4, 2022 · N54241 · Boeing 737800* · Wing Structure
  > B737-57-4-1262-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 NS
- [SDR CALA2022030700573](https://openairdocs.org/sdr/CALA2022030700573.md): Fitting · cracked · Mar 4, 2022 · N54241 · Boeing 737800* · Wing Structure
  > B737-57-4-1262-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 00089
- [SDR CALA2022030700572](https://openairdocs.org/sdr/CALA2022030700572.md): Fitting · cracked · Mar 4, 2022 · N54241 · Boeing 737800* · Wing Structure
  > B737-57-4-1262-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 11
- [SDR CALA2022030700571](https://openairdocs.org/sdr/CALA2022030700571.md): Fitting · cracked · Mar 4, 2022 · N54241 · Boeing 737800* · Wing Structure
  > B737-57-4-1262-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 TRA
- [SDR CALA2022030700570](https://openairdocs.org/sdr/CALA2022030700570.md): Fitting · cracked · Mar 4, 2022 · N54241 · Boeing 737800* · Wing Structure
  > B737-57-4-1262-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 F
- [SDR CALA2022030700569](https://openairdocs.org/sdr/CALA2022030700569.md): Fitting · cracked · Mar 4, 2022 · N54241 · Boeing 737800* · Wing Structure
  > B737-57-4-1262-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 SCR
- [SDR CALA2022030700568](https://openairdocs.org/sdr/CALA2022030700568.md): Fitting · cracked · Mar 4, 2022 · N54241 · Boeing 737800* · Wing Structure
  > B737-57-4-1262-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
- [SDR CALA2022030700567](https://openairdocs.org/sdr/CALA2022030700567.md): Fitting · cracked · Mar 4, 2022 · N54241 · Boeing 737800* · Wing Structure
  > B737-57-4-1262-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 F
- [SDR CALA2022030700566](https://openairdocs.org/sdr/CALA2022030700566.md): Fitting · cracked · Mar 4, 2022 · N54241 · Boeing 737800* · Wing Structure
  > B737-57-4-1262-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 SCIBED
- [SDR CALA2018022100725](https://openairdocs.org/sdr/CALA2018022100725.md): Light · broken · Feb 21, 2018 · N54241 · Boeing 737824 · Emergency Lighting
  > SEAT 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.
- [SDR CALA2018021600656](https://openairdocs.org/sdr/CALA2018021600656.md): Light · inoperative · Feb 16, 2018 · N54241 · Boeing 737824 · Emergency Lighting
  > SEAT 15C EMERGENCY EXIT LIGHT NOT WORKING. THE EMERGENCY LIGHT WAS REPLACED.
- [SDR CALA2017120204291](https://openairdocs.org/sdr/CALA2017120204291.md): Eec · faulty · Dec 2, 2017 · N54241 · Boeing 737824 · Fuel Controlling System
  > ON 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 73

Next page: https://openairdocs.org/aircraft/N54241/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 n_number = 'N54241' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N54241/reports

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