# Service difficulty reports: N27733

A list on [N27733](https://openairdocs.org/aircraft/N27733.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 · 71 reports

- [SDR CALA2026051416226](https://openairdocs.org/sdr/CALA2026051416226.md): Light · inoperative · May 12, 2026 · N27733 · Boeing 737724 · Passenger Compartment Lighting
  > RT OVERWING EMERGENCY DOOR WINDOW LIGHT INOP REMOVED AND REPLACED RH OVERWING EMERGENCY EXIT DOOR WINDOW LIGHT IN REF TO AMM 33-21-00-960-806. OPS CHECK GOOD
- [SDR CALA2026030914451](https://openairdocs.org/sdr/CALA2026030914451.md): Switch · faulted · Mar 6, 2026 · N27733 · Boeing 737724 · Engine Anti-Icing System
  > COWL ANTI-ICE AMBER CAUTION LIGHT CAME ON IN CRUISE. ENGINE WAS IDLED PER QRH. AIRCRAFT PULLED OUT OF SERVICE TROUBLESHOT PER FIM 30-21 TASK 801, UPON INSPECTION FOUND COWL ANTI-ICE CAUTION LIGHT STILL ILLUMINATED. PERFORMED ORIFICE CLEANING IAW AMM 30-21-11-
- [SDR CALA2025100209533](https://openairdocs.org/sdr/CALA2025100209533.md): Access Door · unknown · Oct 2, 2025 · N27733 · Boeing 737724 · Electrical/Electronic Compartment Doors
  > THIS ITEM IS A LEVEL ONE CHRONIC, PLEASE REF FIM'S 52-40 T/801,802 FOR THE FWD ACCESS DOOR AND MAIN E/E DOOR CK BOTH SWITCHES THRU THE PSEU AND ENSURE BOTH ARE ADJUSTED CORRECLY. REF WDM 52-71-12 REMOVE CONN'S D10986/88 FROM THE PSEU CK PIN 6 ON BOTH CONN'S WI
- [SDR CALA2025090408445](https://openairdocs.org/sdr/CALA2025090408445.md): Warning Light · false activation · Aug 26, 2025 · N27733 · Boeing 737724 · Door Warning System
  > EQUIP DOOR ILLUMINTED REPEAT ISSUE. DISCONNECTED WIRES TO DEACTIVATE LIGHT AND VERIFIED EQUIPMENT BAY DOORS ARE CLOSED PER DDP PROCEEDURE *DM* ADDED SW/S197 IN CASE NEEDED. RECOMMEND CHECKING/CLEANING CONNECTIONS AT D10988 AND D10986 REF WDM 52-71-12-1 TO ASS
- [SDR CALA2025080807499](https://openairdocs.org/sdr/CALA2025080807499.md): Window · out of track · Aug 7, 2025 · N27733 · Boeing 737724 · Flight Compartment Windows
  > CA WINDOW NOT INSTALLED CORRECTLY. OUT OF TRACK. FOUND AND REMOVED DEBRIS FROM L2 WINDOW TRACK. INSPECTED L2 WINDOW AND TRACK. NO DEFECTS FOUND. RE-INSTALLED L2 WINDOW PER AMM 56-12-11-400-801. LEAK CHECK GOOD. OK FOR SERVICE.
- [SDR CALA2025061905719](https://openairdocs.org/sdr/CALA2025061905719.md): Deck Plate · buckled · Jun 18, 2025 · N27733 · Boeing 737724 · Fuselage Miscellaneous Structure
  > FLIGHT DECK FLOOR WEB HAS GOUGE REF AAR N/R 9972855
- [SDR CALA2024042201153](https://openairdocs.org/sdr/CALA2024042201153.md): Drain Mast · cracked · Apr 18, 2024 · N27733 · Boeing 737724 · Water and Waste System
  > DURING SERVICE CHECK, WALK AROUND INSPECTION FOUND FWD DRAIN MAST DAMAGE, PERFORMED ADDITIONAL WALK AROUND INSPECTION, NO ADDIDIONAL DEFECTS NOTED. REMOVED AND REPLACED FWD DRAIN MAST REF AMM 38-31-01/401. DRAIN MAST OPS CHECK GOOD.
- [SDR CALA2024041701119](https://openairdocs.org/sdr/CALA2024041701119.md): Windshield · cracked · Apr 15, 2024 · N27733 · Boeing 737724 · Flight Compartment Windows
  > R1 WINDSHIELD ARCED & CRACKED. REMOVED R1 WINDOW IAW AMM 56-11-11-000-801. CHECKED ELEC RESISTANCE OF R1 WINDOW HEAT IAW WDM 30-41-12-1 & CHANGED H13 TB5012-1 TAB NR 1 TO CORRECT NR 2 FOR H12. GLARESHIELD BRACKETS & TRIMS LOCATED AT FIRST CLASS OVERHEAD BIN
- [SDR CALA2024022300518](https://openairdocs.org/sdr/CALA2024022300518.md): Rod · disconnected · Feb 22, 2024 · N27733 · Boeing 737724 · Cargo/Baggage Doors
  > FWD CARGO DOOR LT ON ON INITIAL CLIMB OUT UPON ARRIVAL TO GATE THE FWD CARGO DOOR WAS OPEN. WHEN ATTEMPTING TO CLOSE THE DOOR FOUND THE EXTERIOR HANDLE WOULD NOT TURN THE LATCH ROLLER ARMS ON THE FWD AND AFT SIDE OF THE DOOR. ALL CARGO NETS APPEAR TO BE INTACT
- [SDR CALA2024011700132](https://openairdocs.org/sdr/CALA2024011700132.md): Unknown · unknown · Jan 14, 2024 · N27733 · Boeing 737724 · Engine (Turbine/Turboprop)
  > SLOW SPOOL UP ON NUMBER 2 AFTER STABLE ABOUT 40 TO 50 PERCENT LAG REF. FIM 73-05-00 TASK 814. INSPECTED #2 ENGINE FOR DEFECTS OR DAMAGE. NONE NOTED. PERFORMED EEC BITE CKS. NO FAULTS NOTED. RAN ENGINE AND PERFORMED TEST 8 ACCELERATION CK PER AMM 71-00-00-700-
- [SDR CALA2023102303140](https://openairdocs.org/sdr/CALA2023102303140.md): Unknown · unknown · Oct 20, 2023 · N27733 · Boeing 737724 · Aircraft Fuel System
  > DIVERTED BACK TO KCHS DUE TO POSSIBLE FUEL LEAK IN LEFT ENGINE UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PERFORMED FQIS PER FIM 28-41 TASK 801 NO INFLIGHT FAULTS NO PERFORMED LEFT ENGINE RUN FOR LEAK CK AND LEAK
- [SDR CALA2022123003521](https://openairdocs.org/sdr/CALA2022123003521.md): Control Cable · damaged · Dec 30, 2022 · N27733 · Boeing 737724 · Stabilizer Position Indicating
  > ON TAKEOFF TRIM WAS UNRESPONSIVE- IN NOSE UP-MANUAL TRIM DIDNT WORK//RTB-KCLE. FOUND STAB TRIM CONTROL CABLES FRAYED AT AFT STAB TRIM ACTUATOR. REMOVED AND INSTALLED DAMAGED STA AND STB CABLES INTO THE CABLE RUNS. COMPLETED STAB CONTROL CABLE INSTALLATION.
- [SDR CALA2022072701894](https://openairdocs.org/sdr/CALA2022072701894.md): Compressor · odor · Jul 25, 2022 · N27733 · Boeing 737724 · Potable Water System
  > CABIN CREW REPORTED ODOR ( LIKE RUBBER) IN CABIN ON ARRIVAL. FOUND CAUSE TO BE A FAILED POT WATER COMPRESSOR. REMOVED AND REPLACED POT WATER COMPRESSOR REF TASK 38-42-01-400-801 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1929375 SN OFF 9310 IPC REFERENCE # 38
- [SDR CALA2022041801013](https://openairdocs.org/sdr/CALA2022041801013.md): Position Sensor · inoperative · Apr 18, 2022 · N27733 · Boeing 737724 · Trailing Flap Position Indicating System
  > TRAILING EDGE FLAP DISAGREE ON APPROACH ALT FLAP EXTN LOCKING LGOPAGE UNLOCKING FOR S/O REF LOG8405001,INSTALLED LEFT HAND FLAP POSITION TRANSMITTER REF AMM 27-58-01-400-801. ALL TESTS PASS. ADD EMP:U192656,U221680
- [SDR CALA2022013100271](https://openairdocs.org/sdr/CALA2022013100271.md): Sensor · faulted · Jan 31, 2022 · N27733 · Boeing 737724 · Leading Edge Slat Position Indicating System
  > GOT LE FLAPS TRANSIT LT DURING INITIAL TAKE OFF ROLL. LOW SPEED REJECT HISTORY PREV LEG CREW REPORTS LE FWD LIGHT. #8 SLAT IN TRANSIT BEFORE AND AFTER REMOVED #8 LEADING EDGE SLAT OUTBOARD PROX SENSOR AND MOUNTED ACP SPLICED WIRES IAW SWPM. TAKE OFF ROLL. THEY
- [SDR CALA2021033000397](https://openairdocs.org/sdr/CALA2021033000397.md): Fitting · cracked · Mar 29, 2021 · N27733 · Boeing 737724 · Wing, Attach Fittings
  > SHEAR FITTING AT STA540 LBL6.14 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 6.14 IAW B737- 700 SRM 51-40-02 AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR R EPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, 3/29/202 1 INS
- [SDR CALA2021033000396](https://openairdocs.org/sdr/CALA2021033000396.md): Fitting · cracked · Mar 29, 2021 · N27733 · Boeing 737724 · Wing, Attach Fittings
  > SHEAR FITTING AT STA540 RBL54.60 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 54.60 IAW B737 -700 SRM 51-40-02 AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, 3/29/20 21 IN
- [SDR CALA2021033000395](https://openairdocs.org/sdr/CALA2021033000395.md): Fitting · cracked · Mar 29, 2021 · N27733 · Boeing 737724 · Wing, Attach Fittings
  > SHEAR FITTING AT STA540 LBL32.40 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 32.40 AND SUPP ORT BRACKET. IAW B737-700 SRM 51-40-02 AND UNITED ECRA 5714-0120 5 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPEC TION
- [SDR CALA2021033000394](https://openairdocs.org/sdr/CALA2021033000394.md): Fitting · cracked · Mar 29, 2021 · N27733 · Boeing 737724 · Wing, Attach Fittings
  > SHEAR FITTING AT STA540 RBL40.87 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 40.87. IAW B73 7-700 SRM 41-40-02 AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, 3/29/2 021 I
- [SDR CALA2021033000393](https://openairdocs.org/sdr/CALA2021033000393.md): Fitting · cracked · Mar 29, 2021 · N27733 · Boeing 737724 · Wing, Attach Fittings
  > SHEAR FITTING AT STA540 LBL40.87 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 40.87. IAW B73 7-700 SRM 51-40-02 AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, 3/29/2 021 I
- [SDR CALA2021033000392](https://openairdocs.org/sdr/CALA2021033000392.md): Fitting · cracked · Mar 29, 2021 · N27733 · Boeing 737724 · Wing, Attach Fittings
  > SHEAR FITTING AT STA540 LBL15.04 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 LBL 15.04. IAW B73 7-700 SRM AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, 3/29/2021 INSPECTION C
- [SDR CALA2021033000391](https://openairdocs.org/sdr/CALA2021033000391.md): Fitting · cracked · Mar 29, 2021 · N27733 · Boeing 737724 · Wing, Attach Fittings
  > SHEAR FITTING AT STA540 RBL15.04 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 15.04. IAW B73 7-700 SRM 51-40-02 AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U345651,3/29/20 21 IN
- [SDR CALA2021033000390](https://openairdocs.org/sdr/CALA2021033000390.md): Fitting · cracked · Mar 29, 2021 · N27733 · Boeing 737724 · Wing, Attach Fittings
  > SHEAR FITTING AT ST540 RBL32.40 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 32.40. IAW B73 7-700 SRM 51-40-02 AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, 3/29/2 021 IN
- [SDR CALA2021033000389](https://openairdocs.org/sdr/CALA2021033000389.md): Fitting · cracked · Mar 29, 2021 · N27733 · Boeing 737724 · Wing, Attach Fittings
  > SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED B737-57-4-1262 REMOVED AND REPLACED SHEAR FITTING AT STA 540 RBL 6.14. IAW B737 -70SRM 51-40-02 AND UNITED ECRA 5714-01205 REV ORIGINAL. SSFR RE PORT, FORM 46-0024, ENTERED BY UAL INSPECTION U354651, 3/29/2021 INS
- [SDR CALA2019081091326](https://openairdocs.org/sdr/CALA2019081091326.md): Frame · cracked · Aug 6, 2019 · N27733 · Boeing 737724 · Fuselage Main, Frame
  > LEFT FUSELAGE HAS POSSIBLE START OF CRACK AT I/B RIVET FOR A/C RAIL ATTACH BRACKET STA.380 LEFT BETWEEN S-8LT AND S-9LT.(INDIC ATION WITH HFEC) CUT OUT DAMAGED AREA OF FRAME AND INSTALLED REPAIR DOUBLER PER E C/RA#5310-07648,PART 1.
- [SDR CALA2019080901325](https://openairdocs.org/sdr/CALA2019080901325.md): Bulkhead · canning · Aug 6, 2019 · N27733 · Boeing 737724 · Fuselage Main, Bulkhead
  > APB FOUND TO HAVE AN "OIL CAN" CONDITION BETWEEN STR 2R AND 3RT. REPAIRED APB OIL CANNING BS 1016 BETWEEN S3R AND S5RT.
- [SDR CALA2019081091321](https://openairdocs.org/sdr/CALA2019081091321.md): Frame · cracked · Aug 5, 2019 · N27733 · Boeing 737724 · Fuselage Main, Structure
  > CABIN FRAME CRACKED AT STA.867 RIGHT BETWEEN S-8RT AND S-9RT(I/B RIVET FOR A/C RAIL ATTACH BRACKET)HFEC CONFIRMED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED REPAIR DOUBLER IAW EC/RA 5310-07651,PART 1.
- [SDR CALA2019081091320](https://openairdocs.org/sdr/CALA2019081091320.md): Frame · cracked · Aug 5, 2019 · N27733 · Boeing 737724 · Fuselage Main, Frame
  > CABIN FRAME CRACKED AT STA.380 RIGHT BETWEEN S-8RT AND S-9RT(I/ B RIVET FOR A/C RAIL ATTACH BRACKET) HFEC CONFIRMED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED REPAIR DOUBLER.
- [SDR CALA2019080901319](https://openairdocs.org/sdr/CALA2019080901319.md): Frame · cracked · Aug 5, 2019 · N27733 · Boeing 737724 · Fuselage Main, Frame
  > CABIN FRAME CRACKED AT STA.747 RIGHT BETWEEN S-8RT AND S-9RT(I/B RIVET FOR A/C RAIL ATTACH BRACKET).HFEC CONFIRMED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED REPAIR DOUBLER. ALL WORK ACCOMPLISHED PER EC/RA 5310-07650,PART 1.
- [SDR CALA2019080101279](https://openairdocs.org/sdr/CALA2019080101279.md): Intercostal · punctured · Jul 29, 2019 · N27733 · Boeing 737724 · Fuselage Miscellaneous Structure
  > E&E COMPARTMENT DOOR CUTOUT,INTERCOSTAL WEB AT LBL 6.74 AND BETW EEN STA 323.7 AND 351.2 HAS HOLE PUNCHED IN IT. REPLACED INTERCOSTAL WEB AT LBL 6.74 BETWEEN BS 323.7 & 351.2 RE F SRM 53-10-15,51-40-02,51-40-05,51-20-01 AMM 52-48-41 AND BAC D WG 141A8511,141A8
- [SDR CALA2019080101278](https://openairdocs.org/sdr/CALA2019080101278.md): Bracket · corroded · Jul 29, 2019 · N27733 · Boeing 737724 · Fuselage Miscellaneous Structure
  > SKIN AND FRAME LOCATED BEHIND FWD ACCESSORY DOOR HAS CORROSION U NDER LEVELING COMPOUND BS 277.8 BETWEEN LBL5.7 AND RBL 5.7. REMOVED AND REPLACED CLIP P/N 141A3504-93 AT BS 227.8 BETWEEN LB L5.7 AND RBL 5.7 REF SRM 51-40-02 AND DWG 141A0650 AND REAPPLIED NEW L
- [SDR CALA2018111402371](https://openairdocs.org/sdr/CALA2018111402371.md): Proximity Sensor · faulted · Nov 14, 2018 · N27733 · Boeing 737724 · Leading Edge Slat Position Indicating System
  > LEADING EDGE FLAPS TRANSIT LIGHT STAYS ON 2 PLACED #2 SLAT INDICATION ON MEL 2704E. REMOVED BULBS FROM AMBER INTRANSIT LIGHT ON FWD PANEL. C\W MEL MX PROCEEDURES. FOUND MSG # 27-81202 ON FSEU AND PULLED AND COLLORED C.B. FOR ADD FAULT: 27-81202 INDICATIONS. F
- [SDR CALA2018041601170](https://openairdocs.org/sdr/CALA2018041601170.md): Altimeter · inaccurate · Apr 16, 2018 · N27733 · Boeing 737724 · Altimeter, Barometric/Encoder
  > STANDBY ALTIMETER PROBLEM, STANDBY ALTIMETER STICKS DURING CLIMB AND IS -500 IN CLIMB AND +500 FEET AT FL 370. REMOVED AND REPLACED STANDBY ALTIMETER IAW AMM 34-13-01. OPS CHECKED GOOD.
- [SDR CALA2018041101147](https://openairdocs.org/sdr/CALA2018041101147.md): Frame · cracked · Apr 10, 2018 · N27733 · Boeing 737724 · Fuselage Main, Frame
  > PERFORMED HFEC INSPECTION ON THE RT BS 727 LOWER FRAME, FOUND CRACKED. REPAIRED IAW EA 5310-06135, REV B, OP 005.
- [SDR CALA2018041101146](https://openairdocs.org/sdr/CALA2018041101146.md): Frame · cracked · Apr 10, 2018 · N27733 · Boeing 737724 · Fuselage Main, Frame
  > PERFORMED HFEC AT LT BS 727, LOWER FRAME FASTENER HOLE CRACKED. REPAIRED IAW EA 5310-06135, REV B, OP 004.
- [SDR CALA2017110303919](https://openairdocs.org/sdr/CALA2017110303919.md): Battery · discharged · Nov 3, 2017 · N27733 · Boeing 737724 · Emergency Equipment
  > AFT LT INBD F/A EMERG FLASHLIGHT INOP. REPLACED LT AFT INBD F/A EMERG FLASHLIGHT AND BATTERY. OPS CHECK GOOD.
- [SDR CALA2016122101147](https://openairdocs.org/sdr/CALA2016122101147.md): Circuit Breaker · popped · Dec 21, 2016 · N27733 · Boeing 737724 · Emergency Lighting
  > ON FIRST POWER UP AND EMER EXIT ARMED. EMER EXIT LIGHTS COME ON FROM FRONT OF A/C TO ROW 11. FOUND THE C/B FOR THE EMERGENCY EXIT LIGHT FORWARD CHARGER OUT. ( P18-3 @ A11). C/B RESET LIGHTS OPS CHKS NORMAL.
- [SDR CALA2016062700386](https://openairdocs.org/sdr/CALA2016062700386.md): Skin · damaged · Jun 24, 2016 · N27733 · Boeing 737724 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE OUT LIMITS FROM STA 807 TO STA 847, STR 25L TO STR 27R. REPAIRED IAW ECRA 5331-02109, INITIATED A DIP IAW SAME ECRA PART 1 STEP D-9. ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE JUNE 24, 2018. PLANNING TO CONTACT ENGINEERING AFTER APRI
- [SDR CALA2016062700383](https://openairdocs.org/sdr/CALA2016062700383.md): Skin · damaged · Jun 23, 2016 · N27733 · Boeing 737724 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE FOUND AT STA 471, STR 23L TO STR 24L. ACCOMPLISHED REPAIR OF FUSELAGE SKIN AT STA 471, STR 23L TO STR 24L IAW EC/RA 5331-02104.
- [SDR CALA2016062700382](https://openairdocs.org/sdr/CALA2016062700382.md): Skin · cracked · Jun 23, 2016 · N27733 · Boeing 737724 · Fuselage Main, Plate/Skin
  > REF AD 2013-19-04, EA 5310-05878, REV D, OP-5 STE 7.1 LOWER FUSELAGE STA 540, STR-22, AMP 23, RT SIDE THERE IS A CRACK INDICATION IN THE SKIN AT THE 2 PLACES IN THE FWD FASTENER.2500 HOLE JUST BELOW THE DRAG LINK COMMON TO THE CHORD AREA. FUSELAGE AT STA 540
- [SDR CALA2016062700381](https://openairdocs.org/sdr/CALA2016062700381.md): Skin · cracked · Jun 23, 2016 · N27733 · Boeing 737724 · Fuselage Main, Plate/Skin
  > PERFORMED HFEC IAW NDT PART 6, 51-00-00 PROCEDURE 23 AND EA 530-05878, REV D, STEP 4, 2. FOUND CRACKS ON RT SKIN, STA 540 BETWEEN STR S-22R AND S-23R. CRACK NOTED AT FWD ROW, 2ND HOLE AND CRACK NOTED ON AFT ROW 2ND HOLE. REF FIG 2, SHEET 2 OF 2 OF THE EA NO
- [SDR CALA2013120200884](https://openairdocs.org/sdr/CALA2013120200884.md): Frame · cracked · Nov 30, 2013 · N27733 · Boeing 737724 · Fuselage Main, Frame
  > FRAME 500A LT SHOWS CRACK INDICATION BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE SUPPORT BRACKET FOR AC OUTLET EXTRUSION IAW EA 5310-04716. REPAIRED FRAME STATION 500A LT IAW EA 5310-04716 REV F OP1.
- [SDR CALA2013112700877](https://openairdocs.org/sdr/CALA2013112700877.md): Frame · cracked · Nov 27, 2013 · N27733 · Boeing 737724 · Fuselage Main, Frame
  > FRAME 787L CRACKED BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR AC OUTLET EXTRUSION IAW EA5310-04716. INSTALLED REPAIR AT STATION 787L BETWEEN STRINGER 8 & 9 IAW EA5310-04716 REV F FIG 3.
- [SDR CALA2013112700876](https://openairdocs.org/sdr/CALA2013112700876.md): Frame · cracked · Nov 27, 2013 · N27733 · Boeing 737724 · Fuselage Main, Frame
  > FRAME 727D LT BETWEEN STRINGER 8 & 9 CRACKED AT INBD FASTENER HOLE FOR AC OUTLET EXTRUSION BRACKET IAW EA 5310-04716. INSTALLED REPAIR AT FRAME STATION 727D LT IAW EA A5310-04716 OP 01 REV F FIG 3.
- [SDR CALA2013112700875](https://openairdocs.org/sdr/CALA2013112700875.md): Frame · cracked · Nov 27, 2013 · N27733 · Boeing 737724 · Fuselage Main, Frame
  > FRAME 480R CRACKED BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR AC OUTLET EXTRUSION IAW EA5310-04716. REPAIRED CABIN FRAME STATION 480R IAW EA 5310-04716 OP1 REV F.
- [SDR CALA2013112700874](https://openairdocs.org/sdr/CALA2013112700874.md): Frame · cracked · Nov 27, 2013 · N27733 · Boeing 737724 · Fuselage Main, Frame
  > FRAME 500A RT HAS CRACK BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR SUPPORT BRACKET FOR AC OUTLET EXTRUSION IAW EA 5310-0 4716. REPAIRED CABIN FRAME STATION 500A RT IAW EA 5310-04716 OP1 REV F.
- [SDR CALA2013112700873](https://openairdocs.org/sdr/CALA2013112700873.md): Frame · cracked · Nov 27, 2013 · N27733 · Boeing 737724 · Fuselage Main, Frame
  > FRAME 400R CRACKED BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR AC OUTLET EXTRUSION IAW EA5310-04716. REPAIRED FRAME STATION 400R IAW EA 5310-04716 OP1 REV F.
- [SDR CALA2013112700872](https://openairdocs.org/sdr/CALA2013112700872.md): Frame · cracked · Nov 27, 2013 · N27733 · Boeing 737724 · Fuselage Main, Frame
  > FRAME 727B RT HAS CRACK BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR SUPPORT BRACKET FOR AC OUTLET EXTRUSION REF EA 5310- 04716. REPAIRED CABIN FRAME STATION 727B RT IAW EA 5310-04716 OP1 REV F.
- [SDR CALA2013112700871](https://openairdocs.org/sdr/CALA2013112700871.md): Frame · cracked · Nov 27, 2013 · N27733 · Boeing 737724 · Fuselage Main, Frame
  > FRAME 747L CRACKED BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR AC OUTLET EXTRUSION IAW EA5310-04716. PERFORMED FRAME REPAIR AT STATION 747L BETWEEN STRINGER 8 & 9 IAW EA53 10-04716 OP 01 REV F FIG 3.
- [SDR CALA2013112700870](https://openairdocs.org/sdr/CALA2013112700870.md): Frame · cracked · Nov 27, 2013 · N27733 · Boeing 737724 · Fuselage Main, Frame
  > FRAME 727D RT CRACKED BETWEEN STRINGER 8 & 9 AT INBD FASTENER HOLE FOR AC OUTLET EXTRUSION SUPPORT BRACKET IAW EA 5310-04716. REPAIRED CABIN FRAME STATION 727D RT IAW EA 5310-04716 OP 1 REV F.

Next page: https://openairdocs.org/aircraft/N27733/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 = 'N27733' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N27733/reports

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