# Service difficulty reports: N27239

A list on [N27239](https://openairdocs.org/aircraft/N27239.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 · 97 reports

- [SDR CALA2026101920442](https://openairdocs.org/sdr/CALA2026101920442.md): Lamp · inoperative · Oct 17, 2026 · N27239 · Boeing 737824 · Emergency Lighting
  > RIGHT OVERWING TRAILING EDGE EMERGENCY LIGHT INOPERATIVE. REPLACED THE EMERGENCY LIGHT LAMP IAW AMM 33-51-04-960-801. OPS CHKD GOOD.
- [SDR CALA2026032014707](https://openairdocs.org/sdr/CALA2026032014707.md): Unknown · odor · Mar 19, 2026 · N27239 · Boeing 737824 · Air Distribution System
  > THERE IS A BURNING ELEC TRICAL ODOR NEAR THE FWD GALLEY AND COCK PIT AREA. FAINT ODOR IN THE FRONT OF THE AIRCRAFT, SEEMED TO GO IN AND OUT. NO SMOKE OR ANY OTHER SIGNS OF COMPONENTS OVERHEATING. SMOKE AND ODOR FORM UPLOAD. PERFORMED ECRA 0500-01013 UP TO STEP
- [SDR CALA2026020613617](https://openairdocs.org/sdr/CALA2026020613617.md): Light · inoperative · Feb 5, 2026 · N27239 · Boeing 737824 · Emergency Lighting
  > OPS CHECKED EMERGENCY LIGHTS, UPON INSPECTION EMERGENCY PATHWAY LIGHT INOPERATIVE ROW 20, REPLACED ROW 20 EMERGENCY PATHWAY LIGHT ASSEMBLY, OPS CHECKED GOOD IAW AMM 33-51-11-960-802.
- [SDR CALA2026012613288](https://openairdocs.org/sdr/CALA2026012613288.md): Switch · dirty · Jan 26, 2026 · N27239 · Boeing 737824 · Door Warning System
  > FWD CARGO DOOR LIGHT ON WHILE CLOSED OPENED/CLOSED FWD CARGO DOOR SEVERAL TIMES AND VERIFIED DOOR SWITCH NOT CONTAMINATED WITH ICE OR DEBRIS. NO FIX PLACING FWD CARGO DOOR LIGHT ON MEL. CERIFIED DOOR IS CLOSED AND LOCKED AT THIS TIME. FWD CARGO DOOR WARN IND
- [SDR CALA2025101309972](https://openairdocs.org/sdr/CALA2025101309972.md): Skin · cracked · Oct 11, 2025 · N27239 · Boeing 737824 · Elevator, Plate/Skin
  > PUNCTURE FOUND AT LT ELEVATOR UPPER SURFACE LOCATED 10 INCHES FOR FWD EDGE AND 103 INCHES FROM I/B EDGE. APPLIED PERMANENT REPAIR ON DAMAGED AREA ON LT ELEVATOR UPPER SURFACE LOCATED 10 INCHES FOR FWD EDGE AND 103 INCHES FROM I/B EDGE REF SRM 51-70-04-2R-1 PA
- [SDR CALA2025100709732](https://openairdocs.org/sdr/CALA2025100709732.md): Frame · corroded · Sep 30, 2025 · N27239 · Boeing 737824 · Fuselage Main, Frame
  > FOUND CORROSION AT LT MLG FAILSAFE STRAP EXTERNAL AT STA 663.75 WL199. PERFORMED A REPAIR TO THE OUTER SURFACE OF THE BS 663.75 REAR SPAR BULKHEAD FRAME LT FAILSAFE STRAP NEAR WL 199 IAW AAR-MIA ESR-WI NO.: 2023704-15-12772 AND EC/RA 5340-02240. INITIATE A DI
- [SDR CALA2025100109494](https://openairdocs.org/sdr/CALA2025100109494.md): Attach Angle · cracked · Sep 29, 2025 · N27239 · Boeing 737824 · Fuselage Main, Attach Fittings
  > LEFT VAPOR BARRIER UPPER ATTACHED ANGLE CRACKED AT LBL 7, BS 663. REMOVED AND FABRICATED A NEW UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5, FIGURE 202, DETAIL B, SHT 4.
- [SDR CALA2025092509258](https://openairdocs.org/sdr/CALA2025092509258.md): Deck Plate · damaged · Sep 23, 2025 · N27239 · Boeing 737824 · Fuselage Main, Structure
  > FLIGHT DECK ENTRY FLOOR SKIN CORNER EDGE DAMAGED AT LBL 11, BS 277. REPAIRED FLIGHT DECK ENTRY FLOOR SKIN PANEL CORNER EDGE AT LBL11 STA 277 IAW SRM 53-10-51-2R-2.
- [SDR CALA2025092509252](https://openairdocs.org/sdr/CALA2025092509252.md): Floorbeam · corroded · Sep 23, 2025 · N27239 · Boeing 737824 · Fuselage Main, Floor Beam
  > CABIN AFT WET AREA FLOORBEAM CORRODED BS 967, RBL 16. REPAIR ACCOMPLISHED IAW ESR-WI 2023704-10-12752 AND EC/RA 5370-01193.
- [SDR CALA2025102410502](https://openairdocs.org/sdr/CALA2025102410502.md): Pressure Blkhd · cracked · Sep 13, 2025 · N27239 · Boeing 737824 · Fuselage Main, Bulkhead
  > FOUND CRACK AT BS 1016 AFT PRESSURE BULKHEAD, 2" ABOVE WL 208.1 AND LBL 3. REPAIRED THE DAMAGED AFT PRESSURE BULKHEAD WEB IAW ESR-WI 2023704-24-12817 AND EC/RA 5380-01428,
- [SDR CALA2025100909829](https://openairdocs.org/sdr/CALA2025100909829.md): Floorbeam · corroded · Sep 12, 2025 · N27239 · Boeing 737824 · Fuselage Main, Floor Beam
  > CORROSION CABIN AFT WET AREA FLOORBEAM STA 947.5, LBL9. (REF AAR N/R 97533673) REMOVED THE DAMAGED FLANGES OF THE UPPER TEE OF THE FLOORBEAM BETWEEN LBL 34.5 TO RBL 32.9, INSTALLED NEW TEE ANGLE AND REPAIR PARTS IAW SRM 53-70-51-2R-5 REPAIR 5 WITH THE DEVIA
- [SDR CALA2025092409208](https://openairdocs.org/sdr/CALA2025092409208.md): Floorbeam · corroded · Sep 12, 2025 · N27239 · Boeing 737824 · Fuselage Main, Floor Beam
  > CORROSION ON CABIN AFT WET AREA FLOORBEAM STA 986.5 BETWEEN BL-0 AND RBL 54. REMOVED CORRODED EXISTING TEE CHORD REPAIR AT STA 986.5 FROM RBL 54 TO LBL 50 IAW SRM 51-40-02-0G-0, CUT AND REMOVED THE REMAINING DAMAGE FLANGE FROM LBL 50 TO LBL 54 IAW SRM 53-70-5
- [SDR CALA2025091508909](https://openairdocs.org/sdr/CALA2025091508909.md): Floor Support · cracked · Sep 12, 2025 · N27239 · Boeing 737824 · Fuselage Miscellaneous Structure
  > MAIN CABIN FLOOR SUPPORT WEB CRACKED AT RBL 39 STA 663.75 REMOVED AND CUT THE WEB DAMAGED FROM STA 663.75 BETWEEN RBL38 TO RBL60. INSTALLED NEW WEB AND REPAIR PARTS AT STA 663.75 BETWEEN RBL 30 TO RBL 60 IAW B737 SRM 53-40-51-2R-2 AND SRM 51-40-02-0G-0.
- [SDR CALA2025100709730](https://openairdocs.org/sdr/CALA2025100709730.md): Structure · corroded · Sep 5, 2025 · N27239 · Boeing 737824 · Fuselage Main, Structure
  > CORROSION ON CABIN FWD WET AREA R1 DOOR LOWER INNER CHORD BETWEEN STA 294 AND STA 328. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED INNER CHORD, AT CABIN FWD WET AREA R1 DOOR. LOCATED AND DRILLED NEW INNER CHORD, INSTALLED NEW INNER CHORD AT CABIN FWD WET
- [SDR CALA2025100709729](https://openairdocs.org/sdr/CALA2025100709729.md): Structure · corroded · Sep 5, 2025 · N27239 · Boeing 737824 · Fuselage Main, Structure
  > AFT CABIN STA 986 LBL 55 WEB UNDER L/H INNER CHORD HAS EXFOLIATED CORROSION. REMOVED AND REPLACED WEB AT AFT CABIN STA 986 LBL 55 WEB UNDER L/H INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 147A8501 SHEET 23.
- [SDR CALA2025100709728](https://openairdocs.org/sdr/CALA2025100709728.md): Structure · corroded · Sep 5, 2025 · N27239 · Boeing 737824 · Fuselage Main, Structure
  > AFT PASSANGER CABIN BS 947 LBL 54 (L2 DOOR) INNER CHORD HAS EXFOLIATED CORROSION. REMOVED AND REPLACED INNER CHORD AFT PASSENGER CABIN STA 946 LBL 54" L2 DOOR AS PER SRM 51-40-02-0G-0 AND DWG 147A8501 SHEET 67.
- [SDR CALA2025091508886](https://openairdocs.org/sdr/CALA2025091508886.md): Web · corroded · Sep 5, 2025 · N27239 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CABIN STA 986 RBL 55 WEB UNDER R/H INNER CHORD HAS EXFOLIATED CORROSION. REMOVED AND REPLACED WEB AT AFT CABIN STA 986 RBL 55 UNDER R/H INNER CHORD IAW SRM 51-40-02-G0-0 AND DWG 147A8501 SHEET 25.
- [SDR CALA2025090908633](https://openairdocs.org/sdr/CALA2025090908633.md): Angle · corroded · Sep 5, 2025 · N27239 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD PASSANGER CABIN BS 312 LEFT SIDE (L1 DOOR) INNER CHORD HAS EXFOLIATED CORROSION. REMOVED AND REPLACED FWD PASSANGER CABIN (L1 DOOR) INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 141A8110 SHEET 1.
- [SDR CALA2025090908632](https://openairdocs.org/sdr/CALA2025090908632.md): Structure · corroded · Sep 5, 2025 · N27239 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT PASSANGER CABIN STA 947 RBL 54 (R2 DOOR) INNER CHORD HAS EXFOLIATED CORROSION. REMOVED AND REPLACED INNER CHORD AT AFT PASSENGER CABIN STA 946 RBL 54" (R2 DOOR) IAW SRM 51-40-02-0G-0 AND DWG 147A8501.
- [SDR CALA2025081107549](https://openairdocs.org/sdr/CALA2025081107549.md): Actuator · faulted · Aug 8, 2025 · N27239 · Boeing 737824 · Autopilot Computer
  > THREE UNCOMMANDED RIGHT ROLL INPUTS MADE WHILE ON COMMAND A AUTO PILOT. THE FIRST HAPPENED THRU CHECKED DFCS BITE NO FAULTS NOTED, ALSO CHECKED SMYD COMPUTERS ALSO NO FAULTS NOTED. TEC SUPPORT RECOMMENDS AUTO PILOT A AILERON ACTUATOR REPLACEMENT REMOVED AND R
- [SDR CALA2025072907044](https://openairdocs.org/sdr/CALA2025072907044.md): Cover · detached · Jul 28, 2025 · N27239 · Boeing 737824 · Emergency Lighting
  > 20C EMERGENCY EXIT LIGHTING MISSING FOUND 20C RED EMERG LIGHT COVER MISSING. REPLACED REF MM 33-51-11. OPS CHECK GOOD.
- [SDR CALA2025071806704](https://openairdocs.org/sdr/CALA2025071806704.md): Battery Pack · inoperative · Jul 17, 2025 · N27239 · Boeing 737824 · Emergency Lighting
  > RT WING FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FUSE 4 ON BATTERY PACK M1695. OPS CHECK GOOD. REF AMM 33-51-06.
- [SDR CALA2025041703930](https://openairdocs.org/sdr/CALA2025041703930.md): Lavatory · odor · Apr 17, 2025 · N27239 · Boeing 737824 · Waste Disposal System
  > EXTREME SEWER SMELL ON TAXI OUT OF LGA AND ORD...BOTH FLTS...D ISAPPATE AFTER TAKEOFF.AFT GALLE DEBRIEFED FLIGHT CREW, SPECIFIED SMELL WAS DURING TIME ON APU BLEED, RAN APU AND BLEED AIR MULTIPLE TIMES, NO SMELL NOTED. PER CREW LAV E WAS WORST SMELL, REMOVED
- [SDR CALA2025041503836](https://openairdocs.org/sdr/CALA2025041503836.md): Slide · no discrepancy · Apr 11, 2025 · N27239 · Boeing 737824 · Standard Practices/Structures
  > REMOVED L1 DOOR SLIDE TO F.O.M REINSTALLED ESCAPE SLIDE PACK AND COVER ON L1 DOOR REF AMM 25-66-01-400-803 OPS CHECK GOOD VERIFIED ESCAPE SLIDE PACK AND COVER ON L1 DOOR REF AMM 25-66-01-400-803 OPS CHECK GOOD
- [SDR CALA2024112801343](https://openairdocs.org/sdr/CALA2024112801343.md): Bulb · burned out · Nov 26, 2024 · N27239 · Boeing 737824 · Emergency Lighting
  > RT OVERWING EMERGENCY EX IT LIGHT BURNED OUT PLACED NEW SERVICEABLE BULB IN THE AFT RH OVERWING OUTSIDE PATH LIGHT AS REQUIRED, NO ADDITIONAL DEFECTS NOTED, LIGHT NOW WORKS NORMAL.
- [SDR CALA2024092002458](https://openairdocs.org/sdr/CALA2024092002458.md): Skin · cracked · Sep 7, 2024 · N27239 · Boeing 737824 · Wing, Plate/Skin
  > SUSPECTED CRACK IN LH WING LOWER OUTBOARD SKIN, AT OTBD MOST FASTENER OF S-9 BETWEEN WSTA 564.5 AND WSTA 591.5. INSPECTION VERIFY CRACK IN LH WING LOWER OUTBOARD SKIN PANEL AND STRIPPED PAINT AS REQUIRED IN AREA THAT CRACK WAS FOUND. S-9 CRACK BETWEEN WSTA 564
- [SDR CALA2024091000613](https://openairdocs.org/sdr/CALA2024091000613.md): Tire · failed · Sep 7, 2024 · N27239 · Boeing 737824 · Tire
  > 03 MLG TIRE FOUND BEYOND AMM LIMITS. MUST BE REPLACED PRIOR TO T HE NEXT FLIGHT.#3 MLG TIRE FAILURE REMOVED AND REPLACED NUMBER THREE TIRE IN REF WITH AMM 32-45-11. TEMPORARILY INSTALLED SAFTY BOLTS ON AXLE NUT ON RUNWAY DO TO BAD HARDWARE. NEW CORRECT HARDWAR
- [SDR CALA2023022700558](https://openairdocs.org/sdr/CALA2023022700558.md): Hmu · none · Feb 26, 2023 · N27239 · Boeing 7378 · Engine (Turbine/Turboprop)
  > CREW REPORTED E1 FAILURE DURING CLIMB THRU FL210. ALL TAKE OFF P ARAMETERS NORMAL. ENGINE STARTED SLOW ROLL BACK AT FL210. CREW F LLOWED QRH, SHUT DOWN ENGINE CREW DEBRIEF: NORMAL T/O PARAMETERS; E1 SLOW ROLL BACK REF FIM 73-31 TASK 803 FOR FUEL FLOW WAS NOT D
- [SDR CALA2023022000483](https://openairdocs.org/sdr/CALA2023022000483.md): Skin · corroded · Feb 18, 2023 · N27239 · Boeing 7378 · Fuselage Structure (General)
  > B737-06-3-0026, FUSELAGE EXTERNAL SKIN HAS CORROSION BLISTER AT STA 540 AND BL0. REFER TO PEMCO NR 13291.0282. FEBRUARY 14, 2025. INITIATING DTA DIP PER EC/RA 5330-07054 TO ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF EC/RA 5330-07054 ON OR BEFORE RE-INSP BY Q9
- [SDR CALA2022053001397](https://openairdocs.org/sdr/CALA2022053001397.md): Indicator · unreliable · May 30, 2022 · N27239 · Boeing 737824 · Rate of Climb Indicator
  > AIRSPEED AND ALT UNRELI ABLE AT FL350 F/O INST WERE NOT RELIABL E VISUAL INSPECTION. PUMP THE AIRCRAFT UP AND VERIFY ALL AIRSPEED AND ALT INDICATORS ARE WORKING NORMAL. FO AIRSPEED AND ALT RETURNED TO NORMAL ONCE THEY HIT LOWER TALKED TO CREW THEY REPORTED TH
- [SDR CALA2022040600896](https://openairdocs.org/sdr/CALA2022040600896.md): None · none · Apr 3, 2022 · N27239 · Boeing 737 · Flight Control System
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER CALA2022040600896 SUBMITTED ON 04/06/22. NEAR NO. 3 SLAT ON LOWER EDGE HAS A MISSING PANEL. REPLACED MISSING SLAT PANEL PER EA 00-0592-3-4149. FUNCTION TESTED SLATS ALL FUNCTION TESTED UP AND DOWN OK AT
- [SDR CALA2021100601809](https://openairdocs.org/sdr/CALA2021100601809.md): Pitot System · clogged · Oct 6, 2021 · N27239 · Boeing 737824 · Pitot/Static System
  > REJECTED T/O IAS DISAGRE E JUST AFTER 100 KNOTS A/T FAILED THEN A/S CAPT SIDE REMOVED CAPT AND FO PITOT ADM QUICK DISCONNECT FLUSHED PITOT SYSTEM FOUND MUD DOBBER LOGDGED ON THE CAPT PITOT. CLEARED PITOT SYSTEM LINES AND PERFORMED AIRSPEED LEAK TEST. OPS CHK N
- [SDR CALA2021071401092](https://openairdocs.org/sdr/CALA2021071401092.md): Fire Detector · intermittent · Jul 13, 2021 · N27239 · Boeing 737824 · Fire Detection
  > NO2 ENG OVHT. FOLLOWED QRH. SHUT ENG DOWN CREW DEBRIEF OVERHEAT WAS HIGH NACELLE TEMP. LIGHT. REMOVED AND REPLACED AFT RIGHT ENGINE FIRE DETECTOR ASSEMBLY PER AMM TASK 26-11-01-000-802. OPS CHECKS NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1085427 SN O
- [SDR CALA2021071401091](https://openairdocs.org/sdr/CALA2021071401091.md): Light · broken · Jul 13, 2021 · N27239 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK - FLOOR PROXIMTY LIGHTS ON SEATS 12C AND 29C INOP. REMOVED AND REPLACED WHITE LIGHT ON SEATS 12C & 29C OPS CHECKED GOOD REF. AMM 33-51-11-960-802.
- [SDR CALA2021070901054](https://openairdocs.org/sdr/CALA2021070901054.md): Tire · damaged · Jul 9, 2021 · N27239 · Boeing 737824 · Tire
  > PDA 3 PDA 3 #3 TIRE HAS MISSING CHUNK, WILL TO C/W AMM 05-51-54, AND REPLACE TIRE. ACTIVITIES ACCOMPLISHED INSPECTION REF: MM 05-51-54. CHUNK MEASURES 1/8" DEEP AND 3/4" ROUND. NO DAMAGE NOTED. LOG PAGE 6613853 FOR TIRE CHANGE.
- [SDR CALA2021060700812](https://openairdocs.org/sdr/CALA2021060700812.md): Attach Fitting · missing · Jun 7, 2021 · N27239 · Boeing 737824 · Landing Gear Doors
  > PDA 3 LT MLG FLYING DOOR ATTACH HARDWARE IS COMPLETELY MISSING AT AFT LOWER ATTACH POINT AND THE DOOR IS LOOSE PHOTO ADDED REMOVED LT MLG FLYING DOOR ASSLY (CENTER & INNER DOOR ASSLY) -- REQUEST CDL 32E. DISPATCH DESK: 26 NAME: DK DATE: 06-JUN-21- TOMC APP
- [SDR CALA2021020800144](https://openairdocs.org/sdr/CALA2021020800144.md): Lens · broken · Feb 7, 2021 · N27239 · Boeing 737824 · Emergency Lighting
  > PAX CABIN SEAT 20 L/H RED EMERGENCY LIGHT LENS BROKEN. REF. AAR N/R: 9737524 GENERATED BY: V915555 REMOVED AND REPLACED AT SEAT ROW 20 L/H EMERGENCY LIGHT LENS ( RED) REF. B737 AMM 33-51-11-960-801 AND DRWG#3350DD14973 REV."A" OPERATIONAL TEST NORMAL.REF. AAR
- [SDR CALA2020122801407](https://openairdocs.org/sdr/CALA2020122801407.md): Interphone · failed · Dec 26, 2020 · N27239 · Boeing 737824 · Interphone/Passenger Announcement (PA) System
  > RADIO 2 INOPERABLE COULD NOT HEAR ATC ON COMM 1 OR 2 CAN HEAR/TRANSMIT ON COM 1 IN ALTN MODE ONLY. REMOVED REU PER B737-789 AMM23-51-01-000-801. INSTALLED A SERVICABLE REU, PER B737-789 AMM 23-51-01-000-802 UP TO STEP F. REU INSTALLATION TEST. REU MFG P/N:
- [SDR CALA2020121801401](https://openairdocs.org/sdr/CALA2020121801401.md): Bustle · loose · Dec 17, 2020 · N27239 · Boeing 737824 · Escape Slide
  > ESCAPE SLIDE PACK BUSTLE LOOSE DOOR 1R EXCESS SLIDE MATERIAL BETWEEN BAR AND PACK SHOW ING INSPECTED 1R DOOR ESCAPE SLIDE FOR EXCESS SLIDE MATERIAL BETWEEN BAR AND PACK, FOUND IT NORMAL IN ARMED AND DISARMED POSITION, NO DISCREPANCIES NOTED.
- [SDR CALA2019120902166](https://openairdocs.org/sdr/CALA2019120902166.md): Skin · dented · Dec 6, 2019 · N27239 · Boeing 737824 · Fuselage Main, Plate/Skin
  > FUSELAGE AFT CARGO DOOR CUTOUT UPPER EXTERNAL EDGE HAS A DENT AT BS 794.3 + 8" S-18R + 3" (REF NR 99854117) REPAIRED AFT CARGO DOOR CUT-OUT UPPER EXTERNAL SKIN DENT AT BS794.3 + 8" AND STR 18R + 3" AS PER B737 SRM 53-00-01 FIG 202. ADD EMP:V900430 INSP C/W
- [SDR CALA2019121702220](https://openairdocs.org/sdr/CALA2019121702220.md): Skin · dented · Dec 4, 2019 · N27239 · Boeing 737824 · Fuselage Main, Plate/Skin
  > FOUND DENT IN FUSELAGE SKIN APPROXIMATELY 6" AFT AND 3" ABOVE THE FORWARD CARGO DOOR FORWARD UPPER CUTOUT.NO DMG DOT IN THE AREA. ON OR BEFORE THE AIRCRAFT REACHES 34000 TOTAL AIRCRAFT FLIGHT CY CLES PERFORM AN INSPECTION PER PART 2 OF ECRA 5331-02497. PLANNI
- [SDR CALA2019112862061](https://openairdocs.org/sdr/CALA2019112862061.md): Floorbeam · scratched · Nov 22, 2019 · N27239 · Boeing 737824 · Fuselage Main, Floor Beam
  > FWD CABIN BS 328 FLOOR BEAM HAS SCRATCHED FROM RBL 12 TO RBL 48. (REF NR 99853400) REPAIRED FLOOR BEAM AT STA 328 BL "0" TO RBL 63 AS PER BOEING 737 DRM 53-10-51 REPAIR 7 AND RES 2015289-15 AND EC/RA 5311-02319
- [SDR CALA2019112532033](https://openairdocs.org/sdr/CALA2019112532033.md): Bulkhead Web · cracked · Nov 18, 2019 · N27239 · Boeing 737824 · Fuselage Main, Bulkhead
  > 2EA CRACKS FOUND IN INSPECTION AREA CENTER WING BOX REAR SPAR VE RTICAL PRESSURE WEB BETWEEN RBL40 AND RBL45.64, BETWEEN WL200.6 AND WL192.0, CRACKS MARKED ACCOMPLISHED CATEGORY "B" REPAIR AT CENTER WING BOX REAR SPAR VE RTICAL PRESSURE WEB BETWEEN RBL 40 AND
- [SDR CALA2019112532030](https://openairdocs.org/sdr/CALA2019112532030.md): Floorbeam · corroded · Nov 18, 2019 · N27239 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT CABIN BS 986.5 RBL 43 HAS CORROSION AROUND FASTENER HOLE AS MARKED. [DOT 124-013] REF. AAR N/R: 99853333 REMOVED "TEE" CAP OUT OF LIMITS AT STA 986.5 LBL 38 TO RBL 50. FABRICATED "TEE" CAP AND INSTALLED STA 986.5,LBL 38 RBL 50 AS PER B-737-800 SRM 51-40-02
- [SDR CALA2019111601981](https://openairdocs.org/sdr/CALA2019111601981.md): Rib · cracked · Nov 13, 2019 · N27239 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > LT HORIZONTAL STABILIZER INSPAR RIB 2 - #4 STIFFENER IS CRACKED AT LOWER END. PERFORMED PERMANENT REPAIR L/H HORIZONTAL STAB RIB STA 92.70, #1 STIFFENER IAW B737-800 SRM 55-10-09.REINSTALLED RIB AFTER REPAIR WAS ACCOMPLISHED REF. USED SRM 51-40-02.
- [SDR CALA2019111601980](https://openairdocs.org/sdr/CALA2019111601980.md): Rib · cracked · Nov 13, 2019 · N27239 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > L\H HORIZONTAL STAB RIB AT STA.92.70 #3 STIFFNER CRACKED AT LWR END. REF. AAR N/R: 99853795 ORIGINATED BY EMPLOYEE V915555 PERFORMED PERMANENT REPAIR L/H HORIZONTAL STAB STA 92.70,#3 AND HORIZONTAL STAB RIB STA 92.70 INSTALLATION WILL BE ACCOMPLI SHED ON TASK
- [SDR CALA2019111601979](https://openairdocs.org/sdr/CALA2019111601979.md): Rib · cracked · Nov 13, 2019 · N27239 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > L\H HORIZONTAL STAB RIB AT STA.92.70 #2 STIFFNER CRACKED AT LWR END. REF. AAR N/R: 99853794 ORIGINATED BY EMPLOYEE V915555 PERFORMED PERMANENT REPAIR L/H HORIZONTAL STAB RIB STA 92.70, #2 AND HORIZONTAL STAB RIB STA 92.70 INSTALLATION WILL BE ACCOMPLI SHED ON
- [SDR CALA2019111601978](https://openairdocs.org/sdr/CALA2019111601978.md): Rib · cracked · Nov 13, 2019 · N27239 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > L\H HORIZONTAL STAB RIB AT STA.92.70 #4 STIFFNER CRACKED AT LWR END. REF. AAR N/R: 99853796 ORIGINATED BY EMPLOYEE V915555 PERFORMED PERMANENT REPAIR L/H HORIZONTAL STAB STA 92.70, #4 AND HORIZONTAL STAB RIB STA 92.70 WILL BE ACCOMPLISHED ON TASK CARD # 99854
- [SDR CALA2019111101956](https://openairdocs.org/sdr/CALA2019111101956.md): Rib · cracked · Nov 10, 2019 · N27239 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > R/H HORIZONTAL STABILIZER IN-SPAR RIB STA 101.90 CRACK LOCATED AT TRANSITION RADIUS OF VERTICAL STIFFENER #1. (MKD 126-22) REF. AAR N/R: 99853702 ORIGINATED BY EMPLOYEE V898275 REPAIRED RIB AT STA 101.90 AT #1 VERTICAL STIFFNER AS PER B737- 800 SRM55-10-09 R
- [SDR CALA2019111101955](https://openairdocs.org/sdr/CALA2019111101955.md): Rib · cracked · Nov 9, 2019 · N27239 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > R/H HORIZONTAL STABILIZER IN-SPAR RIB STA 101.90 CRACK LOCATED AT TRANSITION RADIUS OF VERTICAL STIFFENER #3. (MKD 126-024) REF. AAR N/R: 99853705 ORIGINATED BY EMPLOYEE REPAIRED RIB AT STA 101.90 AT SIFFNER #3 AS PER B737-800 SRM 55- 10-09 FIG 202 DETAIL"B

Next page: https://openairdocs.org/aircraft/N27239/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 = 'N27239' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N27239/reports

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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.
