# Service difficulty reports: N54711

A list on [N54711](https://openairdocs.org/aircraft/N54711.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 2 · 90 reports

- [SDR CALA2026080918374](https://openairdocs.org/sdr/CALA2026080918374.md): Skin · dented · Aug 5, 2026 · N54711 · Boeing 737724 · Cargo/Baggage Doors
  > AFT CARGO DOOR HAS MULTIPLE DENTS. REQUEST TO RE-SKIN AFT CARGO DOOR. R & R THE AFT CARGO DOOR EXTERNAL SKIN IAW SRM 52-30-01-2R-3. REMOVED AND REPLACED THE AFT CARGO DOOR EXTERNAL SKIN IAW SRM 52-30-01-2R-3.
- [SDR CALA2026080718347](https://openairdocs.org/sdr/CALA2026080718347.md): Stringer · corroded · Aug 5, 2026 · N54711 · Boeing 737724 · Fuselage Main, Longeron/Stringer
  > E&E BAY, STR-28R WITH CORROSION AT STA 352. REMOVED, LOCATED, DRILLED, APPLIED ALODINE, PRIMER AND INSTALLED NEW STRINGER SPLICE BTW STA 351.50 TO STA 366.01, STR-28R IAW SRM 51-40-02-0G-0, SOPM 20-30-03, AMM 20-60-07-913-801, SRM 51-40-05-0G-0, SRM 51-20-01
- [SDR CALA2026080518274](https://openairdocs.org/sdr/CALA2026080518274.md): Battery Pack · no test · Aug 3, 2026 · N54711 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHTS, BATTERY PACK M1668 FAILED AN OPS CHECK. R & R THE BATTERY PACK M1668 IAW AMM 33-51-06-960-805.
- [SDR CALA2026073118120](https://openairdocs.org/sdr/CALA2026073118120.md): Skin · cracked · Jul 30, 2026 · N54711 · Boeing 737724 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STAB LOWER SKIN, ONE CRACK SIGNAL NOTED AT STA 101.90 I/B SIDE LOCATED TO 10 INCH FWD FROM AFT SPAR. CRACK LENGTH 0.500 INCH. REPAIRED HORIZONTAL STABILIZER LOWER SKIN AT RH SIDE STA 101.90 IAW SRM 55-10-01-2R -11, THIS REPAIR IS A CATEGORY B, R
- [SDR CALA2026072017874](https://openairdocs.org/sdr/CALA2026072017874.md): Rib · cracked · Jul 18, 2026 · N54711 · Boeing 737724 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STAB, STA 92.70 WAS CRACKED IN NR 2 VERTICAL RIB. REPARED THE RIB IAW SRM 55-10-09-2R-4, REPAIR 4 PAR 4 TABLE 201 FIG 202.
- [SDR CALA2026072818066](https://openairdocs.org/sdr/CALA2026072818066.md): Skin · cracked · Jul 17, 2026 · N54711 · Boeing 737724 · Horizontal Stabilizer, Plate/Skin
  > RH HORIZONTAL STAB LOWER SKIN, ONE CRACK SIGNAL NOTED AT STA101.90 I/B SIDE LOCATED TO 10 INCH FWD FROM AFT SPAR. CRACK LENGTH 0.500 INCH. (REF AAR NR 1000086411). REPAIRED HORIZONTAL STABILIZER LOWER SKIN AT RH SIDE STA101.90 IAW B737-700 SRM 55-10-01-2R -11,
- [SDR CALA2026071217706](https://openairdocs.org/sdr/CALA2026071217706.md): Floorbeam · corroded · Jul 11, 2026 · N54711 · Boeing 737724 · Fuselage Main, Floor Beam
  > AFT CABIN FLOORBEAM AT BS 986.5 LT AND RT 6" FR OM BL O HAS CORROSION AND LBL46 REMOVED AND DISCARDED EXISTING REPAIR FABRICATED AND INSTALLED R EPLACEMENT UPPER CHORD REPAIR DETAILS PER 737-700 SRM 53-70-51-2 R-4 AT BS 985.5.
- [SDR CALA2026071217704](https://openairdocs.org/sdr/CALA2026071217704.md): Floorbeam · corroded · Jul 11, 2026 · N54711 · Boeing 737724 · Fuselage Main, Floor Beam
  > M/C STA 946 LBL 53 FLOOR BEAM HAS CORROSION REPAIRED FLOOR BEAM AT STA 946 LBL 53 REF SRM 53-70-51- 2R-5 REPAIR 5. THIS REPAIR IS CATEGORY "A" AND DOES NOT REQUIRE ADDITIONAL INSPECTIONS. ESFR ENTRY. CLEARING LOG PAGE. ALL INFORMATION UPDATED. DMG CARRY NOT
- [SDR CALA2026062517349](https://openairdocs.org/sdr/CALA2026062517349.md): Valve · faulty · Jun 23, 2026 · N54711 · Boeing 737724 · Cabin Cooling System
  > COULD NOT MAINTAIN CABIN TEMP ACCOMPLISHED 700 CABIN TEMP HOT. CABIN TEMP CONTROLLER BITE PASSED. FOUND BAD 35 DEGREE VALVE ON RIGHT PACK. VAVLE OPENS, BUT WONT CLOSE. ALSO, RIGHT CONTROLLER KNOB BROKEN, AND LEFT 35 DEGREE VALVE MISSING POSITION INDICATOR.
- [SDR CALA2026050415948](https://openairdocs.org/sdr/CALA2026050415948.md): Lamp · inoperative · Apr 25, 2026 · N54711 · Boeing 737724 · Emergency Lighting
  > SEAT 26 C BULLNOSE EMERGENCY PATHWAY LIGHT OUT NEEDS ADDITIONAL TROUBLESHOOTING SUSPECT WIRE BUNDLE W00634 BAD, RELAMPED AND REPLACED HOUSING ASSEMBLY STILL NOT WORKING REQUEST MEL 3314A FOR AREA LIGHT INOP BULLNOSE EMERGECY LIGHT MEL 3314A NOT CORRECT MEL RE
- [SDR CALA2025123012517](https://openairdocs.org/sdr/CALA2025123012517.md): Lamp · inoperative · Dec 27, 2025 · N54711 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT OVER EMERGENCY EXIT ON THE RT SIDE IS OUT. RELAMPED ROW 21F EMERGENCY EXIT SIGN, OPS CHECK SATISFACTORY IAW AMM 33-51-01.
- [SDR CALA2025092909383](https://openairdocs.org/sdr/CALA2025092909383.md): Charger · inoperative · Sep 26, 2025 · N54711 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK. EMERGENCY FLOOR ILLUMINATION LIGHTS OUT FROM ROW 3 TO 11. R/R M1676 EMERGENCY LIGHT BATTERY AND CHARGER IAW AMM 33-51-06. OPS CHECK GOOD.
- [SDR CALA2025091208829](https://openairdocs.org/sdr/CALA2025091208829.md): Unknown · odor · Sep 11, 2025 · N54711 · Boeing 737724 · Air Distribution System
  > ENGINE OIL SMELL IN CABIN INBOUND FLIGHT CREW FILLED OUT FORM 46-6020, PERFORMED ENGINE RUN AND APU INDIVDUALLY IN REF TO AMM TASK 05-51-26-800-801-C1, AND FIM 21-00 TASK 806. COULD NOT REPLICATE ODOR ON GROUND, NO HISTORY FOUND PAST 30 DAYS
- [SDR CALA2025081907911](https://openairdocs.org/sdr/CALA2025081907911.md): Oxygen Gen · discharged · Aug 15, 2025 · N54711 · Boeing 737724 · Passenger Oxygen System
  > SEAT 30ABC O2 GENERATOR ACCIDENTLY DISCHARGED. MASKS ARE STOWED REF AMM TASK 35-22-11-400-804-001. COMPLETED REMOVE AND REPLACE OF SEAT 30 ABC O2 GENERATOR. ACCOMPLISHED IDT REQUIREMENTS PER GMM 09-10-05 FOR OXYGEN GENERATOR REPLACEMENT AT ROW 30ABC.
- [SDR CALA2025063006104](https://openairdocs.org/sdr/CALA2025063006104.md): Module · faulted · Jun 26, 2025 · N54711 · Boeing 737724 · Air Data Computer
  > REJECTED T/O AROUND 90 KIAS USING AUTO BRAKES, FOR AIRSPEED DISAGREE F/O IND HAD DISAGR FLAGSVERBAL TURNOVER W/ PILOTS, F/O AIR SPEED STAYED MID 40S KNOTS WITH PILOT SIDE IS AT MID 90S KNOTS, F/O SAID BOTH EEC LIGHT CAME ON, PREFORMED QUICK VISUAL INSPECTION
- [SDR CALA2025021202297](https://openairdocs.org/sdr/CALA2025021202297.md): Oxygen Gen · inoperative · Feb 11, 2025 · N54711 · Boeing 737724 · Passenger Oxygen System
  > ROW 24ABC FOUND PASSENGER OXYGEN GENERATOR PINNED INOPERABLE IN PSU PANEL. REMOVED SHIPPING PIN FROM OXYGEN GENERATOR IAW AMM 35-22-11-400-804-001 AND 35-22-11-400-811-001. ITEM OK FOR SERVICE. VERIFIED SHIPPING PIN REMOVAL FROM OXYGEN GENERATOR IAW AMM 35-22-
- [SDR CALA2025021202296](https://openairdocs.org/sdr/CALA2025021202296.md): Oxygen Gen · inoperative · Feb 11, 2025 · N54711 · Boeing 737724 · Passenger Oxygen System
  > ROW 15ABC FOUND PASSENGER OXYGEN GENERATOR PINNED INOPERABLE IN PSU. REMOVED SHIPPING PIN AND STREAMER FROM GENERATOR IAW AMM 35-22-11-400-804-001 AND 35-22-11-400-811-001. ITEM OK FOR SERVICE. VERIFIED SHIPPING PIN REMOVAL FROM OXYGEN GENERATOR IAW AMM 35-22-
- [SDR CALA2025020302170](https://openairdocs.org/sdr/CALA2025020302170.md): Sign · wrong part · Feb 1, 2025 · N54711 · Boeing 737724 · Emergency Lighting
  > DOOR 112 //1R// EMER EXIT SIGN IS INCORRECT SHOULD NOT HAVE ARRO W REMOVED & REPLACED EMERGENCY EXIT SIGN LIGHT WITH CORRECT SIGN. OP CHK GOOD AT THIS TIME. AC OK TO CONT.
- [SDR CALA2025011701946](https://openairdocs.org/sdr/CALA2025011701946.md): Warning Light · illuminated · Jan 16, 2025 · N54711 · Boeing 737724 · Leading Edge Slat Position Indicating System
  > *EMERGENCY* DECLARED DUE TO LEADING EDGE FLAP TRANSIT LIGHT LEADING FLAP TRANSIT LIGHT QRH FOLLOWED MTC UPDATE TAKEN FROM THE FSEU.. FOUND #2 LH SIDE SLAT OUTBOARD & #7 RH SIDE SLAT OUTBOARD TARGETS BENT WITH AN IN TRANSIT INDICATION AND AS NOTED ON THE FSEU D
- [SDR CALA2024121301499](https://openairdocs.org/sdr/CALA2024121301499.md): Warning Message · illuminated · Dec 11, 2024 · N54711 · Boeing 737724 · Detection System
  > MASTER CAUTION OVERHEAT DETECTOR AND ENGINE 2 OVERHEAT INTERMITTENT. ENGINE IN DICATIONS NORML ACP ENG FIRE CONT MODULE BITE TEST PER AMM 26-10 TASK 801 AND FILGHTDECK ENG FIRE TEST, ALL PASSED. NO HISTORY NOTED, PAST 90 DAYS
- [SDR CALA2024110102765](https://openairdocs.org/sdr/CALA2024110102765.md): Cable · failed · Oct 28, 2024 · N54711 · Boeing 737724 · Drag Control System
  > AFTER TAKEOFF LANDING GEAR FAILED TO RETRACT PAST OFF POSITION O VERWEIGHT LANDING PSEU BITE SHOWS 31-51001 AND 31-52001. HAVE VERIFIED GROUND SPOILER INTERLOCK VALVE CABLE HAS BROKEN UPON FURTHER INSPECTION FOUND GROUND SPOLIER INTERLOCK CABLE INTERLOCK VALVE
- [SDR CALA2024103000964](https://openairdocs.org/sdr/CALA2024103000964.md): Cable · broken · Oct 28, 2024 · N54711 · Boeing 737724 · Drag Control System
  > AFTER TAKEOFF LANDING GEAR FAILED TO RETRACT PAST OFF POSITION O VERWEIGHT LANDING PSEU BITE SHOWS 31-51001 AND 31-52001. HAVE VERIFIED GROUND SPOILER INTERLOCK VALVE CABLE HAS BROKEN UPON FURTHER INSPECTION FOUND GROUND SPOLIER INTERLOCK CABLE BROKEN, REMOVED
- [SDR CALA2024061001741](https://openairdocs.org/sdr/CALA2024061001741.md): Bulb · burned out · Jun 7, 2024 · N54711 · Boeing 737724 · Landing Gear Position and Warning
  > LEFT AND RIGHT PRIMARY GEAR INDICATOR LIGHTS INOP FOUND LEFT MLG LIGHT BURNED OUT. RELAMPED AND TESTED ALL LIGHTS. PERFORMED PSEU BITE TEST PER 32-09 TASK 801 NO EXHISTING FAULTS, NO FAULT HISTORY. ALL GEAR IND LIGHTS OPS CHECK NORMAL. OK TO CONTINUE.
- [SDR CALA2023080402417](https://openairdocs.org/sdr/CALA2023080402417.md): Threshold · unknown · Aug 2, 2023 · N54711 · Boeing 737724 · Fuselage Miscellaneous Structure
  > R2 DOOR THRESHOLD PLATE AREA BOTTOM ROW DOME NUT PIERCED-MARKED REPAIR ACCOMPLISHED BY AERSALE GYR ON NR 003943 CARD 32303 AND DIPS CREATED PER ECRA 5330-07114 ON LP''S 5341676 AND 5341844. RII INSPECTION FOR REPAIR WAS PERFORMED BY AERSALE QC ON NON-ROUTINE 0
- [SDR CALA2023080202400](https://openairdocs.org/sdr/CALA2023080202400.md): Unknown · corroded · Aug 1, 2023 · N54711 · Boeing 737724 · Fuselage Structure (General)
  > FWD ACCY COMPARTMENT STA 227 BL 2R CHORD HAS CORROSION. ON OR BEFORE THE ACCIMULATION OF 50000 TOTAL FLT CYCLES, PERFORM STA 227.8 & RBL 24 AND TO THE REPAIR ON THE SKIN AND BEAR STRAP LATEST REVISION OF ECRA 5311-03042. REF AERSAL EO 5330-23020 AS AN INSPECTI
- [SDR CALA2023080202399](https://openairdocs.org/sdr/CALA2023080202399.md): Skin · dented · Aug 1, 2023 · N54711 · Boeing 737724 · Fuselage Main, Plate/Skin
  > B737-53-3-0731 UPPER FUSELAGE HAS A DENT BETWEEN STA 500C AND 50 0D ON STR 3R. LISHED AT GYR ON WO 003943 CARD # 28707, ON OR BEFORE THE ACCUMU OF THE REPAIR TO THE FUSELAGE SKIN AND STRINGER DENT LOCATED ON PART 2 OF THE LATEST REVISION ECRA 5330-07108. LATIO
- [SDR CALA2023063002099](https://openairdocs.org/sdr/CALA2023063002099.md): Support · worn · Jun 29, 2023 · N54711 · Boeing 737724 · Fuselage Miscellaneous Structure
  > B737-06-3-0053 UPPER RT FUSELAGE TO VERTICAL PANEL SUPPORT WEDGE HAS WEAR STA 1121 REPAIRED UPPER RT FUSELAGE TO VERTICAL PANEL SUPPORT WEDGE PER B 737 SRM 53-80-71-2R-6 REPAIR 6 4.B. DATA WAS TRANSCRIBED FROM AP PER DOC AERSALE WO 3943 OP 28771 BY MECH V92865
- [SDR CALA2023063002098](https://openairdocs.org/sdr/CALA2023063002098.md): Support · worn · Jun 29, 2023 · N54711 · Boeing 737724 · Fuselage Miscellaneous Structure
  > B737-53-3-0731 UPPER LT FUSELAGE TO VERTICAL PANEL SUPPORT WEDGE HAS WEAR AT STA 1121 REPAIRED UPPER LT FUSELAGE TO VERTICAL PANEL SUPPORT WEDGE PERE B737 SRM 53-80-71-2R-6 REPAIR 6 4. DATA WAS TRANSCRIBED FROM PAP ER DOC AERSALE WO 3943 OP 28769 BY MECH V9286
- [SDR CALA2023063002082](https://openairdocs.org/sdr/CALA2023063002082.md): Rib · cracked · Jun 28, 2023 · N54711 · Boeing 737724 · Horizontal Stabilizer, Spar/Rib
  > (SUPPORT TASK) RH HORIZONTAL STAB, STA 92.70 HAS CRACK IN #2 VER TICAL RIB CRIBED FROM PAPER DOC AERSALE WO 3943 OP 32297 BY MECH V942635 I NSP AQC023. REPARED RH HORZ STAB STA 92.70 VERT STIFF ON RIB IAW B737-700 SR M 55-10-09-2R-4 REPAIR 4 PAR 4 TABLE 201 FI
- [SDR CALA2023062301984](https://openairdocs.org/sdr/CALA2023062301984.md): Floorbeam · corroded · Jun 22, 2023 · N54711 · Boeing 737724 · Fuselage Main, Floor Beam
  > (B737-53-3-0737) M/C STA 946 LBL 53 FLOOR BEAM HAS CORROSION
- [SDR CALA2023062101967](https://openairdocs.org/sdr/CALA2023062101967.md): Floor Support · corroded · Jun 20, 2023 · N54711 · Boeing 737724 · Fuselage Structure (General)
  > B737-53-3-0737 AFT CABIN FLOOR BEAM AT BS986.5 L/H AND R/H 6" FR OM BL O HAS CORROSION AND LBL46
- [SDR CALA2023062101966](https://openairdocs.org/sdr/CALA2023062101966.md): Rib · cracked · Jun 20, 2023 · N54711 · Boeing 737724 · Horizontal Stabilizer, Spar/Rib
  > (SUPPORT TASK) LH HORIZONTAL STAB HAS CRACKED #1 VERTICAL STIFFE NER ON RIB AT STAB STA 92.70
- [SDR CALA2023062802042](https://openairdocs.org/sdr/CALA2023062802042.md): Floorbeam · corroded · Jun 19, 2023 · N54711 · Boeing 737724 · Fuselage Main, Floor Beam
  > (B737-53-3-0737) M/C STA 946 LBL 53 FLOOR BEAM HAS CORROSION 43 OP 32036 BY MECH V943916 INSP AQC029. REPAIRED FLOOR BEAM AT STA 946 LBL 53 REF B737-700 SRM 53-70-51- 2R-5 REPAIR 5. DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 39
- [SDR CALA2023062802041](https://openairdocs.org/sdr/CALA2023062802041.md): Floorbeam · corroded · Jun 19, 2023 · N54711 · Boeing 737724 · Fuselage Main, Floor Beam
  > B737-53-3-0737 AFT CABIN FLOOR BEAM AT BS986.5 L/H AND R/H 6" FROM BL O HAS CORROSION AND LBL46 R-4 AT BS 985.5. DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 3943 OP 31836 BY MECH V943919 INSP AQC050. REMOVED AND DISCARDED EXISTING REPAIR FABRICATED AND INST
- [SDR CALA2023061401858](https://openairdocs.org/sdr/CALA2023061401858.md): Unknown · corroded · Jun 14, 2023 · N54711 · Boeing 737724 · Fuselage Structure (General)
  > (SUPPORT TASK) PASSENGER CABIN FLOOR STRUCTURE AT STR 20 RH JUST FWD OF STA 967 RH HAS CORROSION ON THE UPPER HAT FLANGE ON STR 20 RH
- [SDR CALA2022101202781](https://openairdocs.org/sdr/CALA2022101202781.md): Engine · shutdown · Oct 9, 2022 · N54711 · Boeing 737724 · Powerplant System
  > AT FL 410 NUMBER 2 ENG FAILED N1 ROLLED BACK SMALL VIBRATION SO SHUT THE ENGINE DOWN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INSPECT INLET AND EXHAUST AND PROVIDE PICTURES TO UAL TOMC. REMOVED RPL #2 ENG. TT
- [SDR CALA2022052301319](https://openairdocs.org/sdr/CALA2022052301319.md): Speed Switch · loose · May 23, 2022 · N54711 · Boeing 737724 · Central Warning
  > REJECTED TAKEOFF AT 130KNOTS DUE TO TAKEOFF COFIGURATION HORN AND ANNUNCIATION. FOUND SWITCH ASSY SPEEDBRAKE LOOSE, WILL NEED REPLACEMENT ADD EMP:U332357 ACCOMPLISHED FIM 31-51 TASK 803 FOUND SPEED BRAKE TAKE-OFF WARNING SW S651, ACCOMPLISHED TAKE OFF WARNIN
- [SDR CALA2021060200784](https://openairdocs.org/sdr/CALA2021060200784.md): Controller · inoperative · Jun 2, 2021 · N54711 · Boeing 737724 · Cabin Pressure Controller
  > ALT PRESSURIZATION FAIL ON CLIMBOUT. PRESS. PAN- EL BLANKED. CAB IN CLIMB- ED W A/C. CABIN PRESS CONTROLLER #1 SHOWS FAILED. CPC #2 IS OK. ALSO OFV SHOWS FAULT CODE 007 OFV FAILURE THIS CURRENT LEG.PREVIOUS LEGS NO FAULTS. PREVIOUS MEL SHOWS OSV FAULT 011 FAI
- [SDR CALA2020022900540](https://openairdocs.org/sdr/CALA2020022900540.md): Fitting · cracked · Feb 27, 2020 · N54711 · Boeing 737724 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED. -SPT-5866772 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04 IAW ECRA 5714-01100. DATA WAS TRANSCRIBED FROM N/R 5866772, WORK ACCOMPL ISHED BY V900441, INSPECTED BY U354980 INSPECTION ACCEPTED
- [SDR CALA2020022900539](https://openairdocs.org/sdr/CALA2020022900539.md): Fitting · cracked · Feb 27, 2020 · N54711 · Boeing 737724 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED -SPT- 5866766 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 6.14 IAW ECRA 5714-01095. DATA WAS TRANSCRIBED FROM N/R 5866766, WORK ACCOMPLI SHED BY V900441, INSPECTED BY U075598. INSPECTION ACCEPTED
- [SDR CALA2020022900538](https://openairdocs.org/sdr/CALA2020022900538.md): Fitting · cracked · Feb 27, 2020 · N54711 · Boeing 737724 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STA 540 LBL 54.60 IS CRACKED. -SPT-5866769 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 54.60 IAW ECRA 5714-01098.DATA WAS TRANSCRIBED FROM N/R 5866769, WORK ACCOMPLI SHED BY V900441, INWSPECTED BY U075598 INSPECTION ACCEPTED
- [SDR CALA2020022900537](https://openairdocs.org/sdr/CALA2020022900537.md): Fitting · cracked · Feb 27, 2020 · N54711 · Boeing 737724 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED. -SPT-5866767 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 15.04 IAW ECRA 5714-01096. DATA WAS TRANSCRIBED FROM N/R 5866767, WORK ACCOMPL ISHED BY V900441, INSPECTED BY U075598 INSPECTION ACCEPTED
- [SDR CALA2020022900536](https://openairdocs.org/sdr/CALA2020022900536.md): Fitting · cracked · Feb 27, 2020 · N54711 · Boeing 737724 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED. -SPT-5866768 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 40.87 IAW ECRA 5714-01097.DATA WAS TRANSCRIBED FROM N/R 5866768, WORK ACCOMPLI SHED BY V900441, INSPECTED BY U075598 INSPECTION ACCEPTED
- [SDR CALA2020022900535](https://openairdocs.org/sdr/CALA2020022900535.md): Fitting · cracked · Feb 27, 2020 · N54711 · Boeing 737724 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED. -SPT-5866776 REMOVED AND REPLACED SHEAR FITTING AT STA540 RBL 54.6 IAW ECRA 5 714-01103. DATA WAS TRANSCRIBED FROM N/R 5866776, WORK ACCOMPLIS HED BY V900441, INSPECTED BY U075598 INSPECTION ACCEPTED
- [SDR CALA2020022900534](https://openairdocs.org/sdr/CALA2020022900534.md): Fitting · cracked · Feb 27, 2020 · N54711 · Boeing 737724 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED. -SPT-5866775 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 40.87 IAW ECRA 5714-01102. DATA WAS TRANSCRIBED FROM N/R 5866775, WORK ACCOMPL ISHED BY V900441, INSPECTED BY U075598. INSPECTION ACCEPTED
- [SDR CALA2020022900533](https://openairdocs.org/sdr/CALA2020022900533.md): Fitting · cracked · Feb 27, 2020 · N54711 · Boeing 737724 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED. -SPT-5866773 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 32.40 IAW ECRA 5714-01101. DATA WAS TRANSCRIBED FROM N/R 5866773, WORK ACCOMPL ISHED BY V900441, INSPECTED BY U354980 INSPECTION ACCEPTED
- [SDR CALA2020022900532](https://openairdocs.org/sdr/CALA2020022900532.md): Fitting · cracked · Feb 27, 2020 · N54711 · Boeing 737724 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED. -SPT-5866770 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 6.14 IAW ECRA 5714-01099. DATA WAS TRANSCRIBED FRO N/R 5866770, WORK ACCOMPLIS HED BY V900441, INSPECTED BY U075598 INSPECTION ACCEPTED
- [SDR CALA2019071501204](https://openairdocs.org/sdr/CALA2019071501204.md): Light · missing · Jul 15, 2019 · N54711 · Boeing 737724 · Emergency Lighting
  > EMERG EXIT LIGHT MISSING AT SEAT 15C RELAMPED OK. TESTS GOOD.
- [SDR CALA2019053100860](https://openairdocs.org/sdr/CALA2019053100860.md): Sensor · defective · May 29, 2019 · N54711 · Boeing 737724 · Landing Gear Position and Warning
  > WITH GEAR HANDLE UP AFTER TAKEOFF THE NOSE GEAR LIGHT SHOWS GREEN AND RED LIGHT. T/S PER FIM 32-09-00-810-818. BITE SHOWS FAULT 32-61004 LATCHED. INSPECTED S845 AND TB42. FOUND S845 OPEN, SUSPECT SENSOR BAD FROM STOCK. REPLACED TB42 AS PRECAUTION. REF AMM 32-6
- [SDR CALA2019012800178](https://openairdocs.org/sdr/CALA2019012800178.md): Battery Pack · inoperative · Jan 28, 2019 · N54711 · Boeing 737724 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS ON WITH SWITCH IN THE ARM POSITION. REPLACED EMER LT PACK M1668. CORRECTED FAULT AND EMER LTS OPS CK NORMAL REF 33-51-00.

Next page: https://openairdocs.org/aircraft/N54711/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 = 'N54711' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N54711/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.
