# Service difficulty reports: N17229

A list on [N17229](https://openairdocs.org/aircraft/N17229.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 · 103 reports

- [SDR CALA2026101520392](https://openairdocs.org/sdr/CALA2026101520392.md): Power Supply · no test · Oct 14, 2026 · N17229 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS OPS CHECK, RT AFT SLIDE WING EMERGENCY LIGHT INOP. R & R POWER SUPPLY M1671.OPS CHKD NORMAL IAW AMM 33-51-06.
- [SDR CALA2026100820234](https://openairdocs.org/sdr/CALA2026100820234.md): Slide · faulted · Oct 3, 2026 · N17229 · Boeing 737824 · Escape Slide
  > FA REPORTS R2 SLIDE PACK HAS METAL PROTRUDING. REMOVED R2 DOOR ESCAPE SLIDE AND COVER IAW AMM 25-66-01-000-801. INFLATION CYLINDER VALVE SAFETY PIN HAD BEEN INSTALLED. RENDER SAFE CHECKLIST. SLIDE HAS BEEN PLACED IN FWD GALLEY. NINE SCREWS, AND 10 WASHERS T
- [SDR CALA2026081118473](https://openairdocs.org/sdr/CALA2026081118473.md): Light · no test · Aug 10, 2026 · N17229 · Boeing 737824 · Emergency Lighting
  > OPERATIONAL CHECK OF EMERGENCY LIGHTS, RED FLOOR PROXIMITY LIGHT INOPERATIVE AT ROW 20ABC. REPLACED THE LIGHT ASSY IAW AMM 33-51-11. OPS CHKD GOOD. EMERGENCY LIGHTS WORK NORMAL.
- [SDR CALA2026081118472](https://openairdocs.org/sdr/CALA2026081118472.md): Test Button · stuck · Aug 10, 2026 · N17229 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS COME ON IMMEDIATELY BY THEMSELVES. AFT CABIN EMERGENCY LIGHTS DON'T TURN OFF WITH SWITCH IN OFF POSITION. FOUND AFT MODULE M1672 TEST BUTTON STUCK IN TEST MODE. CYCLED BUTTON AND PERFORMED EMERGENCY LIGHT TEST. OPS CHECK NORMAL REFERENCE AMM
- [SDR CALA2026061217043](https://openairdocs.org/sdr/CALA2026061217043.md): Hydraulic Line · leaking · Jun 9, 2026 · N17229 · Boeing 737824 · Hydraulic System, Main
  > LOSS OF SYS A AND B HYDS. REMOVED AND REPLACED HOSE AS PER AMM 32-32-11/401. AFTER HOSE REPLACEMENT, CHECKED SYSTEM FOR LEAKS, ENGINE 1-2 T/R OPS, BRAKES OPS, BLEEDING OF THE MLG ACTUATOR, CHKD HYD CASE DRAIN SYSTEM FILTERS: A AND B, NO PARTICLES FOUND..
- [SDR CALA2026042115554](https://openairdocs.org/sdr/CALA2026042115554.md): Blower · failed · Apr 18, 2026 · N17229 · Boeing 737824 · Weather Radar System
  > WX RADAR NOT WORKING. PAINTS SOLID GREEN ACROSS THE SWEEP IN ARE AS OF KNOWN TSTRMS PERFORMED FIM 34-43 TASK 802. PER CREW BRIEF, NO FAIL MESSAGES OR OTHER FAULTS NOTED. RESET R/T CB AS PRECAUTION. OPERATIONAL CHECK OF WX RADAR NORMAL. REMOVED AND REPLACED WX
- [SDR CALA2026041515370](https://openairdocs.org/sdr/CALA2026041515370.md): Switch · out of position · Apr 12, 2026 · N17229 · Boeing 737824 · Autopilot Computer
  > STAB TRIM AUTOPILOT SWITCH IN CUTOFF POS CREW REPORTED SPEED TRIM FAIL. AIR RETURNED TO IAH UPON MEETING FLIGHT CREW, FOUND AUTOPILOT STAB TRIM IN CUTTOFF POSITION, REF FIM 22-11 TASK 849 PERFORMED SPEED TRIM TEST, ALL TESTS PASSED, NO PREVIOUS HISTORY IN 90 D
- [SDR CALA2025111311180](https://openairdocs.org/sdr/CALA2025111311180.md): Control Valve · out of limits · Nov 11, 2025 · N17229 · Boeing 737824 · Pneumatic Distribution System
  > RIGHT BLEED TRIP OFF LIGHT PERFORMED PNUEMATIC HEALTH CHECK PER MM 36-11-00-700-801. FOUND PRSOV,BAR, AND PRECOOLER CONTROL VALVE OUT OF LIMITS. REMOVED AND REPLACED BAR PER MM 36-11-03. REMOVED AND REPLACED PSROV PER MM 36-11-04. R/R PRECOOLER CONTROL VALVE P
- [SDR CALA2025091608983](https://openairdocs.org/sdr/CALA2025091608983.md): Light · inoperative · Sep 15, 2025 · N17229 · Boeing 737824 · Emergency Lighting
  > ECONOMY PASSENGER SEAT EMERGENCY PATH LIGHTING (EPL) INSPECTION. UPON INSPECTION SEAT ROW 34ABC EMERGENCY PATHWAY LIGHT INOP. REMOVED AND INSTALL NEW EMERGENCY PATHWAY LIGHT ON SEAT ROW 34ABC REF AMM 33-51-11-960-801.
- [SDR CALA2025082808214](https://openairdocs.org/sdr/CALA2025082808214.md): Indication Sys · no discrepancy · Aug 25, 2025 · N17229 · Boeing 737824 · Door Warning System
  > PERFORM AFT ENTRY DOOR INDICATION AND SENSOR TEST (S200) REF. AMM 52-71-11-710-801. PERFORMED AFT ENTRY DOOR INDICATION SENSOR TEST (S200) REF. AMM 52-71-11-710-801. VERIFIED DOOR WARNING SYSTEM IS FUNCTIONING NORMALLY. VERIFIED AFT ENTRY DOOR INDICATION FUNCT
- [SDR CALA2025082708170](https://openairdocs.org/sdr/CALA2025082708170.md): Light · inoperative · Aug 25, 2025 · N17229 · Boeing 737824 · Emergency Lighting
  > RIGHT AFT OVERWING EXTERIOR EMERGENCY LIGHT OUT RELAMPED. RH AFT OVERWING EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECKED GOOD.
- [SDR CALA2025080707438](https://openairdocs.org/sdr/CALA2025080707438.md): Strut · cracked · Aug 6, 2025 · N17229 · Boeing 737824 · Landing Gear Doors
  > RIGHT MLG MID (STRUT) DOOR CRACKED. ACCOMPLISHED REPAIR AT R/H MAIN LANDING GEAR DOOR IAW SRM 52-80-02-2R-3 REPAIR 3.
- [SDR CALA2025080707437](https://openairdocs.org/sdr/CALA2025080707437.md): Strut · cracked · Aug 6, 2025 · N17229 · Boeing 737824 · Landing Gear Doors
  > LEFT MAIN LANDING GEAR MID (STRUT) DOOR CRACKED. ACCOMPLISHED REPAIR AT LT MAIN LANDING GEAR DOOR IAW SRM 52-80-02-2R-3 REPAIR 3.
- [SDR CALA2025081407753](https://openairdocs.org/sdr/CALA2025081407753.md): Window Frame · cracked · Jul 27, 2025 · N17229 · Boeing 737824 · Fuselage Main, Structure
  > RIGHT NR 3 WINDOW FRAME WITH CRACKED FASTENER HOLE (3RD FROM BOTTOM). REPAIRED R3 WINDOW FRAME IAW ESR-WI NO:2023573-13-12408 REV.IR & EC/RA 5310-08660 REV.ORIGINAL,INTERIM REPAIR.
- [SDR CALA2025081407747](https://openairdocs.org/sdr/CALA2025081407747.md): Window Frame · cracked · Jul 27, 2025 · N17229 · Boeing 737824 · Fuselage Main, Structure
  > CRACK FOUND AT L3 WINDOW POST AT HOLE NR 3. CRACKED AT 3 0'CLOCK, CRACK LENGTH - 0.030". REPAIRED L3 WINDOW FRAME IAW ESR-WI NO:2023573-20-12432 AND EC/RA 5310-08653 REV. ORIGINAL, INTERIM REPAIR. PERFORMED THE INTERIM REPAIR TO L3 WINDOW FRAME E-F POST PER
- [SDR CALA2025080107203](https://openairdocs.org/sdr/CALA2025080107203.md): Wedge · delaminated · Jul 27, 2025 · N17229 · Boeing 737824 · Trailing Edge Flaps
  > RIGHT INBD MAIN FLAP OTBD AFT WEDGE WITH EVIDENCE OF DISBONDED. REMOVED AND REPLACED RT INBD MAIN FLAP T/E WEDGE IAW SRM 51-40-02-0G-0, AND DWG 113A2100.
- [SDR CALA2025080107202](https://openairdocs.org/sdr/CALA2025080107202.md): Wedge · corroded · Jul 27, 2025 · N17229 · Boeing 737824 · Trailing Edge Flaps
  > LEFT INBD FLAP OTBD AFT WEDGE WITH EVIDENCE OF A DISBONDED AREA AT TE. REMOVED AND REPLACED LT INBD MAIN FLAP T/E WEDGE IAW SRM 51-40-02-0G-0, AND DWG 113A2100.
- [SDR CALA2025080107201](https://openairdocs.org/sdr/CALA2025080107201.md): Stringer · corroded · Jul 27, 2025 · N17229 · Boeing 737824 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND AT STRINGER 27L, BS 540. REPAIRED STRINGER 27L BETWEEN BS 500I & 540 IAW AAR-MIA ESR-WI 2023573-12-12400, REV IR, AND EC/RA 5330-07571, REV. ORIGINAL.
- [SDR CALA2025080107200](https://openairdocs.org/sdr/CALA2025080107200.md): Frame · cracked · Jul 24, 2025 · N17229 · Boeing 737824 · Fuselage Main, Frame
  > CRACK FOUND AT LT STA 727 FRAME INNER CHORD AT S18A LWR HOLE. ACCOMPLISHED REPAIR AT LOWER AFT FITTING ON LT BS 727 FRAME INNER CHORD AT S18L IAW EC/RA 5310-08657 (ESR-WI 2023573-15-12410)
- [SDR CALA2025072506904](https://openairdocs.org/sdr/CALA2025072506904.md): Fitting · corroded · Jul 24, 2025 · N17229 · Boeing 737824 · APU Cowling/Containment
  > APU COMPARTMENT FITTING LOCATED AT LEFT AND UPPER SIDE SHOWS DAMAGE AT THE EDGE.ACCOMPLISHED REPAIR AT LEFT-HAND APU SUPPORT FITTING IN REF TO EC/RA 5342-01151.
- [SDR CALA2025081407752](https://openairdocs.org/sdr/CALA2025081407752.md): Skin · damaged · Jul 23, 2025 · N17229 · Boeing 737824 · Fuselage Main, Plate/Skin
  > FUSELAGE OUTER SURFACE AT BS 867, S19L EXISTING REPAIR EXTERNAL DOUBLER WITH TOOLING DAMAGE. ACCOMPLISHED REPAIR ON FUSELAGE SKIN AT STA 867 & STR 19L IN REF TO EC/RA # 5331-03175. INTERIM REPAIR.
- [SDR CALA2025081407751](https://openairdocs.org/sdr/CALA2025081407751.md): Spar · corroded · Jul 23, 2025 · N17229 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > CORROSION AT LT HORIZONTAL STAB REAR SPAR LOWER CHORD BOTTOM SURFACE STA 122.5 APROX. ACCOMPLISHED REPAIR AT LEFT LEFT HORIZONTAL STAB REAR SPAR LOWER CHORD SSTA 126 IN REFERENCE TO EC/RA # 5510-03299, CAT B REPAIR.
- [SDR CALA2025072406866](https://openairdocs.org/sdr/CALA2025072406866.md): Seal Depressor · cracked · Jul 21, 2025 · N17229 · Boeing 737824 · Fuselage Main, Structure
  > R1 DOOR CUTOUT UPPER FWD CORNER SEAL DEPRESSOR CRACKED. REMOVED AND REPLACED CORNER SEAL DEPRESSOR AT R 1 DOOR CUTOUT UPPER IAW SRM 51-40-02 SRM AND AIPC 53-11--00-80,TREATED AND APPLIED PRIMER IAW SRM 51-20-01-0G-0 AND AMM 51-21-72-370-804, APPLIED TOP CO
- [SDR CALA2025072106769](https://openairdocs.org/sdr/CALA2025072106769.md): Rib · cracked · Jul 20, 2025 · N17229 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZ STA RIB STA 92.70 STIFFENER #2 WITH CRACK AT LOWER TRANSITION RADIUS. ACCOMPLISHED REPAIR AT RT HORIZ STA RIB STA 92.70 STIFFENER #2 PER SRM 55-10-09-2R-4
- [SDR CALA2025072406865](https://openairdocs.org/sdr/CALA2025072406865.md): Skin · dented · Jul 18, 2025 · N17229 · Boeing 737824 · Cargo/Baggage Doors
  > CUSTOMER REQUEST - REPLACE AFT CARGO DOOR EXTERNAL SKIN. REMOVED AND REPLACED AFT CARGO DOOR SKIN IAW SRM 52-30-01-2R-3, AND DWG 146A6110.
- [SDR CALA2025072406864](https://openairdocs.org/sdr/CALA2025072406864.md): Rib · cracked · Jul 18, 2025 · N17229 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STAB RIB HSS 92.70, STIFFENER NR 1 CRACKED AT LOWER TRANSITION RADIUS. ACCOMPLISHED REPAIR AT RT HORIZ STAB RIB HSS 92.70, STIFFENER NR 1 IAW SRM 55-10-09-2R-5.
- [SDR CALA2025072106754](https://openairdocs.org/sdr/CALA2025072106754.md): Channel · corroded · Jul 18, 2025 · N17229 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD CARGO RIGHT SIDE "Z" CHANNEL IS CORRODED FROM 500D TO 500. REMOVED AND REPLACED FWD CARGO RIGHT SIDE "Z" CHANNEL FROM STA 500B+10 TO STA 500I PER SRM 51-40-02-0G-0 AND DWG#143A7500
- [SDR CALA2025072106753](https://openairdocs.org/sdr/CALA2025072106753.md): Rib · cracked · Jul 18, 2025 · N17229 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > RT HORIZ STA RIB STA 92.70 STIFFENER #4 WITH CRACK AT LOWER TRANSITION RADIUS. ACCOMPLISHED REPAIR AT RT HORIZ STA RIB STA 92.70 STIFFENER #4 PER SRM 55-10-09-2R-4.
- [SDR CALA2025072106752](https://openairdocs.org/sdr/CALA2025072106752.md): Rib · cracked · Jul 18, 2025 · N17229 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > RT HORIZ STA RIB STA 92.70 STIFFENER #3 WITH CRACK AT LOWER TRANSITION RADIUS. REF AAR N/R 9987976 ACCOMPLISHED REPAIR AT RT HORIZ STA RIB STA 92.70 STIFFENER #3 PER SRM 55-10-09-2R-4
- [SDR CALA2025081407749](https://openairdocs.org/sdr/CALA2025081407749.md): Skin · cracked · Jul 16, 2025 · N17229 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT HSS 101.90,10, IN FROM REAR SPAR, I/B ROW. CRACK LENGTH: 0.468IN. ACCOMPLISHED REPAIR AT RT HORIZ STAB LOWER SKIN AT HSS 101.90,10" FROM REAR SPAR, I/B IAW SRM 55-10-01-2R-11 & SRM 51-40-02-0G-0, CAT
- [SDR CALA2025072406863](https://openairdocs.org/sdr/CALA2025072406863.md): Skin · dented · Jul 15, 2025 · N17229 · Boeing 737824 · Cargo/Baggage Doors
  > CUSTOMER REQUEST, REPLACE FWD CARGO DOOR EXTERNAL SKIN AT FWD CARGO DOOR. REMOVED AND REPLACED EXTERNAL SKIN IAW SRM 51-40-02-0G-0, AND DWW 143A6110, APPLIED PAINT IAW AMM 51-21-73-370-803.
- [SDR CALA2025081407748](https://openairdocs.org/sdr/CALA2025081407748.md): Frame · cracked · Jul 12, 2025 · N17229 · Boeing 737824 · Fuselage Main, Frame
  > CABIN FRAME CRACKED AT BS 312 ABOVE L1 DOOR FWD CORNER. REPAIRED FRAME AT MAIN CABIN STA 312 ABOVE L1 DOOR FWD CORNER IAW SRM 53-10-07-2R-1 & SRM 51-40-02-0G-0. CATEGORY "B" REPAIR.
- [SDR CALA2025071406502](https://openairdocs.org/sdr/CALA2025071406502.md): Web · dented · Jul 10, 2025 · N17229 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FLIGHT DECK FLOOR IS DENTED AT B/S 255 14 INCHES LEFT OF CENTER LINE. REF. AAR N/R:9988418. REPAIRED FLIGHT DECK FLOOR WEB BETWEEN STA 250 AND STA 260 FROM LBL 16 TO RBL 2.5 REF B737 SRM 51-40-02-0G-0 AND SRM 53-10-51-2R-2.
- [SDR CALA2025070806344](https://openairdocs.org/sdr/CALA2025070806344.md): Floor Support · cracked · Jul 7, 2025 · N17229 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CABIN FLOOR STRUCTURE INTERCOSTAL RBL 7 STA380-400 WITH CRACKED UPPER ANGLE. REMOVED AND REPLACED FLOOR SUPPORT ANGLE BETWEEN STA380 TO STA 400 RBL7 IAW SRM 51-40-02-0G-0 AND DRW#143A5400.
- [SDR CALA2025070806340](https://openairdocs.org/sdr/CALA2025070806340.md): Rib · cracked · Jul 6, 2025 · N17229 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > LT HORIZ STAB LE 331B WITH CRACKED RIB (2ND FROM IB). REMOVED AND REPLACED RIB AT LT HORIZ STAB LE 331B (2ND FROM IB) PER REF B737-SRM 51-40-02-0G-0 AND DWG NO. 186A1001.
- [SDR CALA2025070806339](https://openairdocs.org/sdr/CALA2025070806339.md): Rib · cracked · Jul 6, 2025 · N17229 · Boeing 737824 · Horizontal Stabilizer, Spar/Rib
  > {B737-06-3-0074} LT HORIZ STAB LE 331B WITH CRACKED RIB (22ND FROM IB). REMOVED AND REPLACED RIB AT LT HORIZ STAB LE 331B (22ND FROM IB) PER REF B737-SRM 51-40-02-0G-0 AND DWG NO. 186A1001.
- [SDR CALA2025070806337](https://openairdocs.org/sdr/CALA2025070806337.md): Rib · worn · Jul 6, 2025 · N17229 · Boeing 737824 · Vertical Stabilizer, Spar/Rib
  > WEAR FOUND AT RIB FIXED LEADING EDGE (FRONT VERTICAL STABILIZER RIB MATTING SURFACE TO THE VERTICAL FIN, 321A, AFT SEAL). REMOVED AND REPLACED FRONT VERTICAL STABILIZER RIB FIXED LEADING EDGE IN REF TO B737 SRM 51-40-02-0G-0 AND 176A3001.
- [SDR CALA2025070806336](https://openairdocs.org/sdr/CALA2025070806336.md): Skin · cracked · Jul 6, 2025 · N17229 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 101.90,10IN FROM REAR SPAR, I/B ROW. CRACK LENGTH: 0.468IN. ACCOMPLISHED REPAIR AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 101.90,10" FROM REAR SPAR, I/B IN REFERENCE TO B737 SRM 55
- [SDR CALA2025070806335](https://openairdocs.org/sdr/CALA2025070806335.md): Floor Support · cracked · Jul 6, 2025 · N17229 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CABIN FLOOR STRUCTURE INTERCOSTAL LBL 13 STA380-400 WITH CRACKED UPPER ANGLE. REMOVED AND REPLACED AT CABIN FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 380 TO STA 400 LBL 13 IAW SRM 51-40-02-0G-0,DWG # 143A5410 SH 16.
- [SDR CALA2025070806334](https://openairdocs.org/sdr/CALA2025070806334.md): Floor Support · cracked · Jul 6, 2025 · N17229 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CABIN FLOOR STRUCTURE INTERCOSTAL BL 0 STA380-400 WITH CRACKED UPPER ANGLE. REMOVED AND REPLACED ANGLE AT CABIN FLOOR STRUCTURE BL 0 AS PER B 737-800 REF SRM 51-40-02-0G-0.
- [SDR CALA2025070806333](https://openairdocs.org/sdr/CALA2025070806333.md): Floorbeam · corroded · Jul 6, 2025 · N17229 · Boeing 737824 · Fuselage Main, Floor Beam
  > FWD WET AREA FLOOR BEAM STA 344 LBL 56 UPPER FLANGE HAS CORROSION. REMOVED CORROSION AT MAIN CABIN FWD WET AREA FLOOR BEAM STA 344 LBL 56 UPPER FLANGE, MEASURED AREA, ORIGINAL MATERIAL 0.175", MATERIAL LOSS 0.063", FOUND OUT OF LIMITS,, CUTOUT DAMAGE AREA B
- [SDR CALA2025070706258](https://openairdocs.org/sdr/CALA2025070706258.md): Floor Support · cracked · Jul 1, 2025 · N17229 · Boeing 737824 · Fuselage Miscellaneous Structure
  > REMOVED AND REPLACED FLOOR SUPPORT AT FWD WET AREA BETWEEN STA 312 TO STA 328 LBL 45.5 IAW SRM 51-40-02-0G-0,DWG # 141A5410. REMOVED AND REPLACED INTERCOSTAL AT FWD WET AREA BETWEEN STA 312 TO STA 328 LBL 45.5 IAW SRM 51-40-02-0G-0,DWG # 141A5410.
- [SDR CALA2025070706257](https://openairdocs.org/sdr/CALA2025070706257.md): Floor Support · corroded · Jul 1, 2025 · N17229 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD WET AREA INTERCOASTAL BETWEEN STA 328 TO STA 344 LBL 44 HAS CORROSION. REMOVED CORROSION, FOUND OUT OF LIMITS, LOCATED AND DRILLED NEW INTERCOSTAL STA328 TO STA344 LBL 45.5, IAW SRM 51-40-02-0G-0, 53-10-51-1A-1 AND THIS IS BEING INSTALLED ON WORK CARD 9
- [SDR CALA2025070306190](https://openairdocs.org/sdr/CALA2025070306190.md): Structure · corroded · Jul 1, 2025 · N17229 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD WET AREA L/H SIDE INNER CHORD HAS CORROSION FROM STA 328 TO STA 344. COMPLETED INSTALLATION AT FWD WET AREA OF L1 DOOR INNER CHORD IAW SRM 51-40-02-0G-0 DWG # 141A8110.
- [SDR CALA2025062605913](https://openairdocs.org/sdr/CALA2025062605913.md): Floor Support · corroded · Jun 24, 2025 · N17229 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT WET AREA R/H SIDE INNER CHORD BETWEEN STA 947 TO STA 987 HAS SEVERAL SPOTS CORRORED. REMOVED AND REPLACED R2 DOOR INNER CHORD IN REF B 737-800 SRM 51-40-02-0G-0 AND DWG# 147A8501.
- [SDR CALA2025062605912](https://openairdocs.org/sdr/CALA2025062605912.md): Floor Support · corroded · Jun 24, 2025 · N17229 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD WET AREA R/H SIDE INNER CHORD HAS CORROSION FROM STA 312 TO STA 344. REMOVED AND REPLACED INNER CHORD AT FWD WET AREA R/H SIDE REF. SRM 51-40-02-0G-0 & DWG # 141A8310.
- [SDR CALA2025062605898](https://openairdocs.org/sdr/CALA2025062605898.md): Floorbeam · corroded · Jun 23, 2025 · N17229 · Boeing 737824 · Fuselage Main, Floor Beam
  > AFT WET AREA FLOOR BEAM STA 987 RBL 43 UPPER FLANGE HAS CORROCION. ACCOMPLISHED FLOOR BEAM REPAIR AT AFT WET AREA STA 986.5 RBL 43 IN REF SRM 53-70-51-2R-6 REPAIR 6.
- [SDR CALA2025070806328](https://openairdocs.org/sdr/CALA2025070806328.md): Angle · corroded · Jun 22, 2025 · N17229 · Boeing 737824 · Fuselage Miscellaneous Structure
  > FWD WET AREA R-1 CENTER THRESHOLD SUPPORT HAS CORROSION AROUND FASTENER HOLE STA 312+ 11" RBL58.DOT251-007 REF AAR N/R 9987991 REMOVED AND REPLACED THRESHOLD SUPPORT AT FWD WET AREA FLOOR STRUCTURE R1 DOOR RBL 58 IAW SRM 51-40-021-0G-0,DWG # 141A8310, N
- [SDR CALA2025062305821](https://openairdocs.org/sdr/CALA2025062305821.md): Floor Support · corroded · Jun 22, 2025 · N17229 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT WET AREA INTERCOASTAL BETWEEN BS 947 - 967, RBL 50 UPPER FLANGE HAS CORROCION AROUND FASTENER HOLE. REMOVED AND REPLACED INTERCOSTAL AT AFT WET AREA BETWEEN BS 947 - 967, RBL 50 IAW SRM 51-40-02-0G-0 AND DWG 147A5760.
- [SDR CALA2025071506572](https://openairdocs.org/sdr/CALA2025071506572.md): Floor Support · corroded · Jun 21, 2025 · N17229 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR PANEL SUPPORT STA 987+6 LBL 36 HAS CORROCION. REMOVED AND INSTALLED PANEL SUPPORT AT AFT WET AREA STA 987+6 LBL 36 IN REFERENCE TO B737 SRM 51-40-02-0G-0. STEP 4.B.

Next page: https://openairdocs.org/aircraft/N17229/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 = 'N17229' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N17229/reports

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