# Service difficulty reports: N12225

A list on [N12225](https://openairdocs.org/aircraft/N12225.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 · 83 reports

- [SDR CALA2025120811825](https://openairdocs.org/sdr/CALA2025120811825.md): Light · broken · Dec 6, 2025 · N12225 · Boeing 737824 · Emergency Lighting
  > FLOOR LEVEL EMERGENCY EX IT LIGHT ON 24C DISCONNECTED FROM SEAT FOUND BROKEN ON LIGHT HOUSING BROKEN. NO OTHER EMERGENCY AISLE LIGHT INOPERATIVE. PLACING 24C EMERGENCY AISLE LIGHT ON MEL. MEL 3315A REJECT FOR SIGNOFF REPLACED 24C EMERGENCY LIGHT HOUSING. OPS C
- [SDR CALA2025120411766](https://openairdocs.org/sdr/CALA2025120411766.md): Warning Light · false activation · Dec 1, 2025 · N12225 · Boeing 737824 · Door Warning System
  > MASTER CAUTION DOORS REJECTED TAKEOFF 115KTS NO LIGHT ON OVERHEAD. PERFORMED A HIGH ENERGY STOP INSPECTION IAW AMM 05-71-07, NO DEFECTS NOTED. GVI FOUND FWD SERVICE DOOR SWITCH JAM NUT LOOSE. TIGHTENED JAM NUT AND SECURED IAW AMM 52-71-11-802-801. FWD SVC DOO
- [SDR CALA2025102810669](https://openairdocs.org/sdr/CALA2025102810669.md): Controller · faulted · Oct 25, 2025 · N12225 · Boeing 737824 · Cabin Pressure Controller
  > CABIN ALT WARNING AT 290. CREW STATED AT 29000FT CABIN ALTITUDE WARNING DISPLAYED, CABIN CLIMB RATE SHOWING 1000FT PER MINUTE WHILE LEVELED OFF AT 290, DURING DESCENT AT 6000FT CABIN PRESSURE INDICATION SHOWING 30000FT. R & R NR 1 & 2 CABIN PRESSURE CONTROLLER
- [SDR CALA2025060905376](https://openairdocs.org/sdr/CALA2025060905376.md): Floorbeam · corroded · Jun 4, 2025 · N12225 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT WET AREA FLOOR STRUCTURE BEAM AT STA 947.5 LBL 4 WITH CORROSION AT UPPER SURFACE AROUND FASTENER HOLE. REF AAR N/R 9967557 ACCOMPLISHED REPAIR AT FLOOR BEAM UPPER CHORD STA 947.5 AT LBL 4.0 REFERNCE AAR-MIA ESR-WI NO;2023385-24-12086 EC/RA 5370-01173 S REV
- [SDR CALA2025053005123](https://openairdocs.org/sdr/CALA2025053005123.md): Rib · cracked · May 28, 2025 · N12225 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > [EA 5510-01843 REV H OP 002] L/H HORIZONTAL STABILIZER IN-SPAR RIB FOUND 2 CRACKS AT STAB STA 101.90 BEHIND #1 STIFFENER. REF AAR N/R 9967192 REPAIRED LH HORIZONTAL STAB IN-SPAR RIB STA 101.90 ON BEHIND #1 STIFFENER IN REF TO SRM 55-10-09-2R-5, FIG 203..
- [SDR CALA2025052905077](https://openairdocs.org/sdr/CALA2025052905077.md): Structure · corroded · May 23, 2025 · N12225 · Boeing 737824 · Fuselage Main, Structure
  > MAIN CABIN AFT WET AREA FOUND EVIDENCE OF CORROSION ON THE INNER CORD AT STA. 967.5 LBL 47.5. INSTALLED INNER CHORD AT STA 897 TO STA 1006 LBL 62 IAW DWG # 147A8501 AND B737-800, SRM51-40-02-0G-0.
- [SDR CALA2025052905076](https://openairdocs.org/sdr/CALA2025052905076.md): Floorbeam · corroded · May 23, 2025 · N12225 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT WET AREA FOUND EVIDENCE OF CORROSION ON THE INNER CORD AT STA. 986.5 RBL 47.5 REMOVED AND REPLACED R2 INNER CHORD AT AFT WET AREA FLOOR STRUCTURE RBL 47.5 PER SRM 51-40-02-0G-0, DWG# 147A8501, AND DWG #147A0000.
- [SDR CALA2025052704968](https://openairdocs.org/sdr/CALA2025052704968.md): Support Angle · damaged · May 23, 2025 · N12225 · Boeing 737824 · Fuselage Miscellaneous Structure
  > LOWER FUS SUPPORT ANGLE WORN R/H O/B OF RAM AIR EXIT EXHAUST DUCT AFT STA 663.75. REMOVED AND REPLACED SUPPORT ANGLE AT LOWER FUS. R/H O/B OF RAM AIR EXIT EXHUST DUCT STA 663.75 IAW B737-800, SRM 51-40-02-0G-0, AND DRW #149A7216.
- [SDR CALA2025052704966](https://openairdocs.org/sdr/CALA2025052704966.md): Fitting · cracked · May 23, 2025 · N12225 · Boeing 737824 · Wing Main, Frame Structure
  > RIGHT WING REAR SPAR DEFLECTION CONTROL RIB O/B BEAM FITTING UPPER TAB IS CRACKED. REMOVED AND REPLACED SUPPORT ANGLE AT LOWER FUS. R/H O/B OF RAM AIR EXIT EXHUST DUCT STA 663.75 IAW B737-800, SRM 51-40-02-0G-0, AND DRW #149A7216
- [SDR CALA2025052905073](https://openairdocs.org/sdr/CALA2025052905073.md): Stiffener · cracked · May 22, 2025 · N12225 · Boeing 737824 · Fuselage Main, Bulkhead
  > LEFT W/W FWD BULKHEAD STIFFENER CRACKED AT LOWER REDIUS STA 663.75 LBL 25. REMOVED AND REPLACED STIFFENER ON LEFT W/W FWD BULKHEAD STA 663.75 LBL 25 REF. B737-800, SRM 51-40-02-0G-0 AND DWG #111A1000.
- [SDR CALA2025052905072](https://openairdocs.org/sdr/CALA2025052905072.md): Skin · cracked · May 22, 2025 · N12225 · Boeing 737824 · Leading Edge Devices
  > LEFT WING MOVEABLE SLAT#4 ASSY L/E LOWER SKIN LOOSE FASTENERS WITH ELONGATED HOLES AT ACTUATOR ATTACHMENT RIB. TRIMMED OUT DAMAGED SKIN AREA AND INSTALLED REPAIR ON LEFT WING SLAT#4 BOTTOM L/E SKIN REF SRM 57-42-01-2R-8.
- [SDR CALA2025052905070](https://openairdocs.org/sdr/CALA2025052905070.md): Skin · cracked · May 20, 2025 · N12225 · Boeing 737824 · Leading Edge Devices
  > RIGHT WING MOVEABLE L/E SLAT ASSY # 5 L/E LOWER SKIN FASTENERS LOOSE WITH ELONGATED HOLES AT ACTUATOR ATTACHED RIB. TRIMMED OUT DAMAGED AREA AND ACCOMPLISHED REPAIR AT SLAT #5 LOWER SKIN REF. B737-800, SRM 57-42-01-2R-8.
- [SDR CALA2025052104890](https://openairdocs.org/sdr/CALA2025052104890.md): Angle · cracked · May 20, 2025 · N12225 · Boeing 737824 · Fuselage Miscellaneous Structure
  > RT AIR CONDITIONER BAY TO VAPOR BARRIER AFT UPPER ANGLE CRACKED AROUND MOST IB ATTACH FASTENER. REF. AAR N/R:9967538 GENERATED BY:V919797 ESFR INFORMATION ENTERED. ESFR ENTERED BY STEVE AST U180628 C/W
- [SDR CALA2025052004852](https://openairdocs.org/sdr/CALA2025052004852.md): Depressor · cracked · May 19, 2025 · N12225 · Boeing 737824 · Fuselage Main, Structure
  > R1 DOOR FWD UPPER CORNER DEPRESSOR CRACKED.
- [SDR CALA2025052905069](https://openairdocs.org/sdr/CALA2025052905069.md): Floorbeam · corroded · May 17, 2025 · N12225 · Boeing 7378 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT WET AREA FOUND EVIIDENCE OF CORROSIONON ON THE BEAM UPPER SURFACE OF THE T CORD AT STATION 986.5 RBL 44. INSTALLED REPAIR ON FLOOR BEAM UPPER SURFACE T- CHORD AT STA 986.5 RBL 44 REF. ECRA #5321-01429 REV. H.
- [SDR CALA2025052905067](https://openairdocs.org/sdr/CALA2025052905067.md): Floorbeam · corroded · May 16, 2025 · N12225 · Boeing 737824 · Fuselage Main, Floor Beam
  > FWD WET AREA FLOOR STRUCTURE FOUND CORROSION ON FLOOR BEAM AT STA 344 LBL55". REF AAR N/R 9966926 UPDATE ESFR INFO INSTALLED REPAIR TO THE STA 344 TRANSVERSE FLOOR BEAM UPPER CHORD PER AAR- MIA ESR-WI NO.: 2023385-17-12057 AND UNITED EC/RA #5310-08567 EV. W
- [SDR CALA2025052004843](https://openairdocs.org/sdr/CALA2025052004843.md): Frame · gouged · May 16, 2025 · N12225 · Boeing 737824 · Fuselage Main, Frame
  > MAIN CABIN L/H LOWER SIDEWALL FRAME LOWER AFT EDGE SMALL GOUGE STA 663.75 S-16L. REF. AAR N/R:9967378 REF. AAR N/R:9967376. WRONG N/R:9967378 USED.
- [SDR CALA2025051904785](https://openairdocs.org/sdr/CALA2025051904785.md): Web · corroded · May 16, 2025 · N12225 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR STRUCTURE BEAM AT STA 947.5 LBL 4 WITH CORROSION AT UPPER SURFACE AROUND FASTENER HOLE. ACCOMPLISHED REPAIR ON STA 947.5 LBL 4 AS PER ESR-WI 24-12086 P1 REMOVED AND REPLACED WEB AT STA 986.5 TO 1016 LBL32" IAW B737 SRM 51-40-02, AND DRW
- [SDR CALA2025051904783](https://openairdocs.org/sdr/CALA2025051904783.md): Angle · corroded · May 16, 2025 · N12225 · Boeing 737824 · Fuselage Miscellaneous Structure
  > REMOVED AND REPLACED ZEE ANGLE AT AFT WET AREA AT INTERCOASTAL AREA STA 987 TO 1006 IAW SRM 51-40-02-0G-0 FOR REF AAR N/R 9966931 UPDATE LP TO REFLECT ESFR REMOVED AND REPLACED ZEE ANGLE AT AFT WET AREA AT INTERCOASTAL AREA STA 987 TO 1006 IAW SRM 51-40-02-0G-
- [SDR CALA2025051904782](https://openairdocs.org/sdr/CALA2025051904782.md): Frame · gouged · May 16, 2025 · N12225 · Boeing 737824 · Fuselage Main, Frame
  > MAIN CABIN R/H LOWER SIDEWALL FRAME LOWER FWD EDGE SMALL GOUGE STA 663.75 S-16R MKD DOT 137 (REF AAR N/R 9967377) ESFR INFORMATION ADDED ESFR COMPLETE WORK ACCOMPLISHED BY U422520
- [SDR CALA2025052905066](https://openairdocs.org/sdr/CALA2025052905066.md): Frame · cracked · May 15, 2025 · N12225 · Boeing 737824 · Fuselage Main, Frame
  > CABIN FRAME AT STA 480 BETWEEN S8L AND S9L WITH EVIDENCE OF CRACK AT CLEVIS IB ATTACH FASTENER. INSTALLED REPAIR AT MAIN CABIN FRAME STA 480 BETWEEN S8LTO S9L REF. B737-800 SRM 51-40-02-0G-0, AND UNITED EC/RA #5310-07665 REV. ORIGINAL
- [SDR CALA2025051604732](https://openairdocs.org/sdr/CALA2025051604732.md): Stub Frame · cracked · May 15, 2025 · N12225 · Boeing 737824 · Fuselage Main, Frame
  > CRACK FOUND AT INTERNAL FWD GALLEY DOOR STUB FRAME UPPER FWD SKIN S-8R (CRACK LENGTH.400") (REF AAR N/R 9967428)
- [SDR CALA2025052905064](https://openairdocs.org/sdr/CALA2025052905064.md): Floorbeam · corroded · May 14, 2025 · N12225 · Boeing 737824 · Fuselage Main, Floor Beam
  > MAIN CABIN AFT WET AREA FOUND EVIIDENCE OF CORROSIONON ON THE UPPER SURFACE OF THE T CORD AT STATION 986.5 LBL 43.5 INSTALLED REPAIR AT FLOOR BEAM STA 986.5 RBL 20" TO LBL 49" REF. B737 SRM 53-70-51-2R-4, AAR ESR-WI #14-12044, AND EC/RA #5370-01175.
- [SDR CALA2025052905063](https://openairdocs.org/sdr/CALA2025052905063.md): Frame · cracked · May 13, 2025 · N12225 · Boeing 737824 · Fuselage Main, Frame
  > FWD CABIN FUS ATTACHED FRAME CUTOUT SMALL CRACK ABOVE L-1 DOOR.
- [SDR CALA2025053005118](https://openairdocs.org/sdr/CALA2025053005118.md): Skin · corroded · May 11, 2025 · N12225 · Boeing 737824 · Fuselage Main, Plate/Skin
  > L/H LOWER FUS SKIN FOUND BULGING CORROSSION AT DIAGONAL ATTACHED ANGLE APPROX S-21L STA 540. REF. AAR N/R:9967393ESFR CREATED AND SENT ACCOMPLISHED REPAIR AT WING CENTER SECTION FWD LWR SKIN PANEL REF. AAR ESR-WI #2023385-22-12079 AND EC/RA 5710-02928 REV. ORI
- [SDR CALA2025060205164](https://openairdocs.org/sdr/CALA2025060205164.md): Stringer · corroded · May 10, 2025 · N12225 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > SUPPORT TASK MAIN E/E COMPARTMENT SKIN PANEL VERY LIGHT SURFACE CORR AT O/B S-25L BETWEEN STA 344 AND STA 396MKD DOT 149 REF AAR N/R 9967474 SSFR SUBMITTED BY T RIGUERO V894534 INSTALLED REPAIR AT MAIN E/E COMPT S-25L BETWEEN 360 AND STA 380 REF B737 SRM 53-00
- [SDR CALA2025051204603](https://openairdocs.org/sdr/CALA2025051204603.md): Skin · cracked · May 9, 2025 · N12225 · Boeing 737824 · Leading Edge Devices
  > RT WING #7 SLAT LE LOWER SKIN CRACKED AT ACTUATOR ATTACHING AREA AROUND FASTENER HOLE. REPAIR PERFORMED ON AAR N/R 9966752-6000-0036 CUT OUT DAMAGED AREA AND INSTALLED REPAIR AT SLAT #7 LOWER SKIN IN REF B737-800 SRM 57-42-01-2R-8.
- [SDR CALA2025050704525](https://openairdocs.org/sdr/CALA2025050704525.md): Floorbeam · corroded · May 5, 2025 · N12225 · Boeing 737824 · Fuselage Main, Floor Beam
  > CABIN FWD WET AREA FLOOR BEAM AT STA 380 BETWEEN LBL 51 - LBL 64 WITH SURFACE CORROSION SPOT. REMOVED CORROSION AT MAIN CABIN FWD WET AREA FLOOR BEAM 380 LBL 57 IAW SRM 51-10-02-0G-0,& PERFORMED REPAIR PER AAR ESR-WI REV IR #2023385-15-12049,AND UNITED EC/RA
- [SDR CALA2025052905062](https://openairdocs.org/sdr/CALA2025052905062.md): Stringer · corroded · May 4, 2025 · N12225 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > MAIN E/E COMPARTMENT FLOOR BILGE CORROSION AT S-27R STA 360. TRIMMED OUT DAMAGED STRINGER SECTION AND INSTALLED STRINGER AND SPLICE REPAIR BETWEEN STA 360 TO STA 400 STR 27R REF. B737-800 SRM 53-00-03-2R-1.
- [SDR CALA2025051204597](https://openairdocs.org/sdr/CALA2025051204597.md): Stringer · corroded · May 4, 2025 · N12225 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > MAIN E/E COMPARTMENT FLOOR BILGE CORROSION AT S-28R STA 360 REF AAR N/R 9967573. REMOVED AND REPLACED MAIN E/E COMPARTMENT FLOOR BILGE STRINGER AT S-28R STA 360 TO STA 400 PER IAW 737-800 IN REFERENCE SRM 53-00-03-2R-1.REF.AAR N/R:9967573.
- [SDR CALA2025050604487](https://openairdocs.org/sdr/CALA2025050604487.md): Rib · cracked · May 4, 2025 · N12225 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > R/H HORIZONTAL STABILIZER IN-SPAR RIB FOUND A CRACK AT STAB STA 92.70 BEHIND #1 STIFFENER. FOR REF AAR N/R 9967391 SFR INFORMATION ADDED REPAIRED RH HORIZONTAL STAB IN-SPAR RIB STA 92.7 ON STIFFENER #1 IN REF TO SRM 55-10-09-2R-5.
- [SDR CALA2025050504455](https://openairdocs.org/sdr/CALA2025050504455.md): Rib · cracked · May 4, 2025 · N12225 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > AS PER EA 5510-01843 REV H OP 002 R/H HORIZONTAL STABILIZER IN-SPAR RIB FOUND A CRACK AT STAB STA 92.70 ON #2 STIFFENER. REPAIRED RH HORIZONTAL STAB IN-SPAR RIB STA 92.7 ON STIFFENER #2 IN REF TO SRM 55-10-09-2R-4.
- [SDR CALA2025050504443](https://openairdocs.org/sdr/CALA2025050504443.md): Skin · dented · Apr 30, 2025 · N12225 · Boeing 737824 · Cargo/Baggage Doors
  > REMOVE AND REPLACE FWD CARGO DOOR EXTERNAL SKIN. REMOVED AND REPLACED FWD CARGO DOOR EXTERNAL SKIN PER SRM 51-40-02-0G-0 SRM 52-30-01-2R-3 AND DWG#143A6110.
- [SDR CALA2025050504441](https://openairdocs.org/sdr/CALA2025050504441.md): Skin · dented · Apr 30, 2025 · N12225 · Boeing 737824 · Cargo/Baggage Doors
  > REMOVE AND REPLACE AFT CARGO DOOR SKIN REF AAR N/R 9967429 ADDED SFR INFO REMOVED AND REPLACED AFT CARGO DOOR EXTERNAL SKIN PER SRM 52-30-01-2R-3 AND DWG#146A6110 WORK ACCOMPLISHED BY V939559 ESFR NO.:821 INSP C/W
- [SDR CALA2025032002991](https://openairdocs.org/sdr/CALA2025032002991.md): Switch · broken · Mar 18, 2025 · N12225 · Boeing 737824 · Emergency Lighting
  > EMERGENCY EXIT LITES CAME ON DURING INITAL CLIMB. THEN TURNED OFF ON THEIR OWN FOUND GUARD-SWITCH FOR EMERGENCY LIGHT SWITCH AT AFT FLT. ATTEND. PANEL MISSING. IPC 33-51-01-56, ITEM #10, PN: 2100-11, M&E: 19-3351-3-0014. GUARD-SWITCH. AMM 33-51-00-710-004. IN
- [SDR CALA2025022402449](https://openairdocs.org/sdr/CALA2025022402449.md): Warning Light · false indication · Feb 21, 2025 · N12225 · Boeing 737824 · Door Warning System
  > AFT ENTRY DOOR LIGHT ILLUMINATED AT ABOUT 90 KNOTS UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID MAC RELATED WORK ORDER 000000003130133. DEBRIEFED THE CREW AND FOUND THE DOO
- [SDR CALA2024062400066](https://openairdocs.org/sdr/CALA2024062400066.md): Skin · gouged · Jun 20, 2024 · N12225 · Boeing 737824 · Fuselage Main, Plate/Skin
  > FOUND DENT AND GOUGE ON LT AFT FUSELAGE JUST BEHIND PRESSURIZED AREA. APPROX STA 1040 STGR 11-12. PERFORMED REMOVAL OF DAMAGE PER SRM 53-80-01 REPAIR 7 REMOVAL OF DAMAGE. COMPLIED WITH STEP 4F HFEC INSPECTION REF NDT PART 6-51-00-00-23 OF CUTOUT EDGE, NO CRAC
- [SDR CALA2023070502162](https://openairdocs.org/sdr/CALA2023070502162.md): Motor · inoperative · Jul 3, 2023 · N12225 · Boeing 737824 · Stabilizer Position Indicating
  > STAB TRIM INOP CONFIRMED ALL 3 CBS - C2, B10, D10 WERE IN ON ARRIVAL TO NOTE: STABLILIZER CONTROL TRIM WHEEL DIFFICULT TO MOVE MANUALLY. AIRCRAFT. PERFORMED STABILIZER ELECTRIC TRIM SYSTEM TEST REF AMM OFFERS LOTS MORE RESISTANCE THAN NORMAL 27-41-00-700-803,
- [SDR CALA2023042101199](https://openairdocs.org/sdr/CALA2023042101199.md): Flap · stuck · Apr 20, 2023 · N12225 · Boeing 7378 · Trailing Edge Flap Control System
  > SELECTED FLAPS 30 AND FLAPS STAYED AT 25. WENT AROUND AND NEXT APPCH FLAPS WENT TO 30. ACCOMPLISHED OPERATIONAL TEST OF FLAPS/ SLATS TEST IS OK.GROUNDS TEST FLAPS/ SLATS CSU NO FAULTS REF AMM 27-58-01-820-801
- [SDR CALA2022103103002](https://openairdocs.org/sdr/CALA2022103103002.md): Skin · damaged · Oct 30, 2022 · N12225 · Boeing 737824 · Fuselage Main, Plate/Skin
  > AFT FUSELAGE EXTERNAL SKIN DAMAGED 4.24" FWD OF TAIL SKID BL 0. REF BY PEMCO NR. 12810.0717. EVALUATED AFT FUSELAGE EXTERNAL SKIN FWD OF TAIL SKID FOUND TO B E OUT OF LIMITS OUT OF LIMITS PER B737-800 SRM 53-00-011A-1 REPA IRED AREA IAW B737-800 SRM 53-80-01-2
- [SDR CALA2022010500026](https://openairdocs.org/sdr/CALA2022010500026.md): Light · damaged · Jan 4, 2022 · N12225 · Boeing 737824 · Passenger Compartment Lighting
  > SEAT MOUNTED EMERGENCY EXIT LIGHT AT 30ABC DAMAGED. REMOVED AND REPLACED WHITE LIGHT ASSY REF MM 33-51-11. OPS CK OK. VERIFIED IDT REQUIREMENTS
- [SDR CALA2022010500025](https://openairdocs.org/sdr/CALA2022010500025.md): Light · damaged · Jan 4, 2022 · N12225 · Boeing 737824 · Passenger Compartment Lighting
  > SEAT MOUNTED EMERGENCY EXIT LIGHT AT 22ABC DAMAGED. REMOVED AND REPLACED WHITE LIGHT ASSY REF MM 33-51-11. OPS CK OK. VERIFIED IDT REQUIREMENTS
- [SDR CALA2019082601435](https://openairdocs.org/sdr/CALA2019082601435.md): Failsafe · corroded · Aug 24, 2019 · N12225 · Boeing 737824 · Fuselage Main, Structure
  > FWD CARGO COMPARTMENT FRAME 500D, FAIL SAFE CHORD CORROSION AT S TR 24L. REFERENCE D2 CHECK NR # 99843232. REPAIRED PER ECRA 5311-02234. PER ECRA PART 1(E.
- [SDR CALA2019080431298](https://openairdocs.org/sdr/CALA2019080431298.md): Skin · cracked · Aug 2, 2019 · N12225 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND AT LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STAB STA 101.90 APPROXIMATELY 11.000" FWD FROM TRAILING EDGE OF SKIN. APPROXIMATE CRACK LENGTH: 0.625". (REF NR 99842797) REPAIRED L/H HORIZONATAL STABILIZER LOWER SKIN, IN-SPAR SKIN AT S
- [SDR CALA2019011300071](https://openairdocs.org/sdr/CALA2019011300071.md): Cover · out of position · Jan 10, 2019 · N12225 · Boeing 737824 · Passenger/Crew Doors
  > AFTER TAKEOFF LOUD AIR NOISE COMING FROM DOOR 1L LOOKED LIKE LOW ER HINGE COVER WAS OUT TALKED TO INBOUND CREW, FOUND THAT DOOR 1L AT LOWER HINGE COVER OF LOWER GUIDE ARM STUCK ON INSIDE OF DOOR BUSTLE AREA. RELIEVED STUCK AREA OF HINGE SEAL BRAKET AREA AND S
- [SDR CALA2018081701799](https://openairdocs.org/sdr/CALA2018081701799.md): Not Reported · lack of lube · Aug 11, 2018 · N12225 · Boeing 737824 · Flight Control System
  > AIRCRAFT DIFFICULT TO CONTROL IN THE ROLL AXIS. FELT LIKE MANUAL REVISION. HYD NORMAL, AP OF OIL SERVICE ACCOMPLISHED. PREFORMED FIM 27-11-00-810-804, AND AMM 27-11-810-804, LUBRICATED ALL POINTS FROM THE FLIGHT DECK TO THE WHEEL WELL. FOUND NO BINDING OK F
- [SDR CALA2018020900555](https://openairdocs.org/sdr/CALA2018020900555.md): Lamp · inoperative · Feb 9, 2018 · N12225 · Boeing 737824 · Emergency Lighting
  > LEFT EXTERIOR FUSELAGE EMERGENCY LIGHT AFT OF LT WING FOUND INOPERATIVE DURING AN 2SVC. REPLACED THE LAMPS IAW MM 33-51-04, OPS CHECKED OK.
- [SDR CALA2017071002167](https://openairdocs.org/sdr/CALA2017071002167.md): Lens · missing · Jul 10, 2017 · N12225 · Boeing 737824 · Emergency Lighting
  > EMERGENCY EXIT LIGHT LENS MISSING AT ROW 21DEF. R & R EMERGENCY EXIT LIGHT ASSY. OPS CHECKED NORMAL. OK TO CONTINUE IN SERVICE.
- [SDR CALA2017070102078](https://openairdocs.org/sdr/CALA2017070102078.md): Lens · missing · Jul 1, 2017 · N12225 · Boeing 737824 · Emergency Lighting
  > OVERHEAD EMERGENCY EXIT SIGN OVER AISLE AT ROW 25 IS MISSING. REINSTALLED LIGHT LENS COVER IAW AMM 33-51-01. OK FOR SERVICE.
- [SDR CALA2017020300253](https://openairdocs.org/sdr/CALA2017020300253.md): Lamp · inoperative · Feb 3, 2017 · N12225 · Boeing 737824 · Emergency Lighting
  > SLIDE OVERWING LIGHT DOES NOT COME ON, REPLACED THE LAMPS CHECKED NORMAL

Next page: https://openairdocs.org/aircraft/N12225/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 = 'N12225' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N12225/reports

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