# Service difficulty reports: N12218

A list on [N12218](https://openairdocs.org/aircraft/N12218.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 · 102 reports

- [SDR CALA2026080518284](https://openairdocs.org/sdr/CALA2026080518284.md): Battery · discharged · Aug 4, 2026 · N12218 · Boeing 737824 · Emergency Equipment
  > FWD FLASHLIGHT BLINKING RED AND INOP. FOUND FLASHLIGHT BATTERY DISCHARGED. REPLACED BATTERY AND RESEALED. OPS CHECKED NORMAL.
- [SDR CALA2026052616542](https://openairdocs.org/sdr/CALA2026052616542.md): Skin · corroded · May 18, 2026 · N12218 · Boeing 737824 · Fuselage Main, Plate/Skin
  > CORROSION ON LWR CENTER WNG SKIN OB SIDE ON RIGHT DRAG LINK 2" AFT OF WING FRONT SPAR. (REF AAR N/R 100019659)ACCOMPLISHED REPAIR AT WING CENTER SECTION FORWARD LOWER SKIN PANEL INTERIM REPAIR STA 540 AS REQUIRED PER ECRA #5710-02979, COMPLIANCE WITH THE REQUI
- [SDR CALA2026052616540](https://openairdocs.org/sdr/CALA2026052616540.md): Window Frame · cracked · May 16, 2026 · N12218 · Boeing 737824 · Fuselage Main, Structure
  > EA 5310-08195 REV C OP 003 - OPERATION 003 - AS REQUIRED PER STEP 26 ITEM IS BEING GENERATED FOR EGNINEERING PURPOSES FOUND CRACK ON FASTENER HOLE # 2 CURRENT DIMENSION.424" AND CRACK ON #3 HOLE CURRENT DIMENSION.300" REQUIRE FURTHER ASSISTANCE. REF AAR N/R 1
- [SDR CALA2026052116430](https://openairdocs.org/sdr/CALA2026052116430.md): Housing · gouged · May 15, 2026 · N12218 · Boeing 737824 · Cargo/Baggage Doors
  > FWD CARGO DOOR EXTERANAL HANDLE HOUSING GOUGED. REMOVED AND REPLACED HANDLE HOUSING AT FWD CARGO DOOR IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, & DWG 143A6110.
- [SDR CALA2026051716305](https://openairdocs.org/sdr/CALA2026051716305.md): Support Frame · gouged · May 15, 2026 · N12218 · Boeing 737824 · Aerodynamic Fairings
  > LEFT SIDE FUSELAGE WING-TO-BODY FAIRING SUPPORT AT APPROXIMATELY STA 727 JUST ABOVE FLAP TRACK #4 GOUGED. ACCOMPLISHED REPAIR AT LEFT SIDE FUSELAGE WING-TO-BODY FAIRING SUPPORT FRAME AT STA 727 JUST ABOVE FLAP TRACK #4 AS REQUIRED PER ECRA # 5360-02141, COMP
- [SDR CALA2025110911020](https://openairdocs.org/sdr/CALA2025110911020.md): Slide · unpacked · Nov 6, 2025 · N12218 · Boeing 737824 · Escape Slide
  > DOOR 1L SLIDE MATERIAL IS HANGING FROM BOTTOM OF DOOR. REINSTALLED EXCESS HANGING SLIDE MATERIAL. OK FOR CONTINUED SERVICE. REF AMM 25-66-01/401 VERIFIED RII REQUIREMENTS FOR 1L SLIDE REINSTALL PER GMM 09-25-05 & AMM 25-66-01-400-803.
- [SDR CALA2025110911019](https://openairdocs.org/sdr/CALA2025110911019.md): Girt Bar · excess play · Nov 6, 2025 · N12218 · Boeing 737824 · Emergency Equipment
  > DOOR 1R GIRT BAR FLAP HAS EXCESS MATERIAL. REINSTALLED EXCESS HANGING SLIDE MATERIAL. OK FOR CONTINUED SERVICE. IAW AMM 25-66-01/401. VERIFIED RII REQUIREMENTS FOR 1R SLIDE REINSTALL PER GMM 09-25-05 & AMM 25-66-01-400-803.
- [SDR CALA2025100209535](https://openairdocs.org/sdr/CALA2025100209535.md): Disk · broken · Oct 2, 2025 · N12218 · Boeing 737824 · Crew Oxygen System
  > O2 GREEN DISK BROKEN. REPLACED BROKEN DISCHARGE INDICATOR DISK IAW AMM 35-12-51.
- [SDR CALA2025092209090](https://openairdocs.org/sdr/CALA2025092209090.md): Bulkhead Web · cracked · Sep 17, 2025 · N12218 · Boeing 737824 · Fuselage Main, Bulkhead
  > LEFT HAND UPPER PRESSURE DECK IS CRACKED AT STA 640 AND RBL 35 JUST ABOVE GROUND SPOILER CONTROL VALVE. ADDING PHOTOS OF CRACKED AREA, CRACK IS ON RHS OF AC. COMPLETED REPAIR ACCOMPLISHED IAW SRM 53-40-51-2R-2 PG 1-10 FIG 202. REMOVED AND CUT THE WEB DAMAGE
- [SDR CALA2025091608981](https://openairdocs.org/sdr/CALA2025091608981.md): Light · detached · Sep 10, 2025 · N12218 · Boeing 737824 · Emergency Lighting
  > SEAT 30ABC EMERGENCY AISLE LIGHT DETACHED FROM FRAME REQUESTING MEL, ALL OTHER EMERGENCY LIGHTS ARE OPERATIVE TOMC APPROVED REMOVED EMERGENCY EXIT FLOOR AISLE LIGHT AND SECURED WIRES. COMPLIED WITH MAINTENANCE FUNCTION IAW MEL CARD 3319E. OK FOR SERVICE. INS
- [SDR CALA2024121201488](https://openairdocs.org/sdr/CALA2024121201488.md): Fire Detector · faulty · Dec 9, 2024 · N12218 · Boeing 737824 · Fire Detection
  > ENG 2 OVERHEAT LIGHT LIGHT IS ON ENG 2 OVRHT ILLUMINATED ON CLIMBOUT. WENT OUT AFTER LVL OFF CHEC KLIST THRUST REDUCTION UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. FOUND WIRE CHAFFED NEAR CONNECTOR. WIRE NOT DA
- [SDR CALA2024082602267](https://openairdocs.org/sdr/CALA2024082602267.md): Connector · broken · Aug 23, 2024 · N12218 · Boeing 737824 · Light System Wiring
  > EMERGENCY LIGHT ON SEAT ROW 15ABC IS INOP.(WARRANTY)SUPPORT TASK NSA EMX N/R 00196. REMOVED AND REPLACED MATE-N-LOK CONNECTOR FOR SEAT ROW 15ABC EEPL LIGHT AND OPS CHECK GOOD IAW AMM 33-51-00, SWPM 20-42-01, AND CMM 25-22-55.
- [SDR CALA2024080702176](https://openairdocs.org/sdr/CALA2024080702176.md): Seat Track · broken · Aug 3, 2024 · N12218 · Boeing 737824 · Fuselage, Seat/Cargo Attach Fittings
  > BETWEEN F.S. 540-560 R/H O/B SEAT TRACK HAS BROKEN LOBE. SUPPORT TASK NSA EMX N/R 00087.
- [SDR CALA2023052901681](https://openairdocs.org/sdr/CALA2023052901681.md): Skin · deformed · May 26, 2023 · N12218 · Boeing 737824 · Fuselage Main, Plate/Skin
  > R/H FUSELAGE STA 259.5 STR 20R LEADING EDGE OF SKIN DOUBLER REPAIR IS BENT/ CONTOUR IS DEFORMED. 43 AND BS 277, S-18R AND S-23R IN ACCORDANCE WITH PART 2 OF ECRA CYCLES. NOTE TO PLANNING: THIS ECRA IS BEING EVAL. FOR DAMAGE TO INSPECTION CRITERIA WILL BE INCLU
- [SDR CALA2023052601663](https://openairdocs.org/sdr/CALA2023052601663.md): Skin · damaged · May 25, 2023 · N12218 · Boeing 737824 · Fuselage Main, Plate/Skin
  > REFERENCE L/P 4677633. FOR INTERIM SKIN REPAIR AT STATION 500H-540 STR 26L-26R. REQUIRES 2ND DTA DIP NOTE TO PLANNING: THIS EC/RA IS BEING EVALUATED FOR DAMAGE SUPPLEMENTAL INSPECTIONS. THE INSPECTION CRITERIA WILL BE TOLERANCE. UNDER 14CFR 26.43(D) WHICH WILL
- [SDR CALA2023052601657](https://openairdocs.org/sdr/CALA2023052601657.md): Frame · corroded · May 25, 2023 · N12218 · Boeing 737824 · Fuselage Main, Frame
  > AREA AFT OF FORWARD CARGO COMPARTMENT IN A/C BAY, FORWARD SIDE OF STA 540 BULKHEAD HAS LOWER FRAME BULGING DUE TO CORROSION AT BL-0 BETWEEN S-28L AND S-28R JUST AFT OF INTERNAL SIDE OF EXTERNAL A/C ATTACHMENT OPENING AS SHOWN. SEE ATTACHED. BULKHEAD CHORD REPA
- [SDR CALA2023052601656](https://openairdocs.org/sdr/CALA2023052601656.md): Skin · corroded · May 25, 2023 · N12218 · Boeing 737824 · Fuselage Main, Plate/Skin
  > SKIN AT EXTERNAL A/C CONNECTION CORRODED AND PULLING THROUGH FASTENERS. SEE ATTACHED IMAGES FUSELAGE SKIN REPAIR IN ACCORDANCE WITH PART 2 OF EC/RA 5330-07087 ON OR BEFORE 20 MAY 2025 PERFORMED INTERIM REPAIR PER EC/RA 5330-07087 AT STA 500H-540 LOWER SKIN. PL
- [SDR CALA2023052601667](https://openairdocs.org/sdr/CALA2023052601667.md): Skin · corroded · May 24, 2023 · N12218 · Boeing 737824 · Fuselage Main, Plate/Skin
  > SKIN AT EXTERNAL A/C CONNECTION CORRODED AND PULLING THROUGH FASTENERS. SEE ATTACHED IMAGES FUSELAGE SKIN REPAIR IN ACCORDANCE WITH PART 2 OF EC/RA 5330-07087 ON OR BEFORE 20 MAY 2025 PERFORMED INTERIM REPAIR PER EC/RA 5330-07087 AT STA 500H-540 LOWER SKIN. PL
- [SDR CALA2023052601665](https://openairdocs.org/sdr/CALA2023052601665.md): Frame · corroded · May 24, 2023 · N12218 · Boeing 737824 · Fuselage Main, Frame
  > AREA AFT OF FORWARD CARGO COMPARTMENT IN A/C BAY, FORWARD SIDE OF STA 540 BULKHEAD HAS LOWER FRAME BULGING DUE TO CORROSION AT BL-0 BETWEEN S-28L AND S-28R JUST AFT OF INTERNAL SIDE OF EXTERNAL A/C ATTACHMENT OPENING AS SHOWN. SEE ATTACHED. BULKHEAD CHORD REPA
- [SDR CALA2023052201600](https://openairdocs.org/sdr/CALA2023052201600.md): Skin · cracked · May 20, 2023 · N12218 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > L/H HORIZONTAL STABILIZER LOWER SKIN ACCESS HOLES WAS CUT TO REPAIR CRACKED RIB AT STATION 92.70 REFERENCE BAM N/R EXTERNAL DOUBLER AND EXTERNAL LFEC INSP AND REINSPECTION AT 9000 PER TABLE 204 OF SRM 55-10-01/2R01 REPAIR 11-SFR #D9182 CREATED- END FL CYCLES
- [SDR CALA2023030600639](https://openairdocs.org/sdr/CALA2023030600639.md): Chain · none · Mar 6, 2023 · N12218 · Boeing 7378 · Stabilizer Position Indicating
  > TRIM WHEEL IS MAKING A GRINDING SOUND WHEN THE ELECTRIC TRIM IS IN OPERATION UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PERFORMED PRECAUTIONARY INSPECTION OF HORZ. STAB. CABLES, PULLEYS, AND DRUM CABLE IN AFT J
- [SDR CALA2022100302634](https://openairdocs.org/sdr/CALA2022100302634.md): Pump · faulty · Oct 3, 2022 · N12218 · Boeing 737824 · Hydraulic Power Accumulator, Main
  > ENG 1 ENGINE HYD PUMP LOW PRESSURE LIGHT ILLUMINATED INFLIGHT. FLUID DOWN TO 20. INSTALLED #1 ENGINE HYD PUMP, LEAK COMPLETED A SYSTEM HYD FLUSHING, RAN ENGINE NO LEAKS. AIRCRAFT OK TO CONTINUE.
- [SDR CALA2022091202338](https://openairdocs.org/sdr/CALA2022091202338.md): None · missing · Sep 12, 2022 · N12218 · Boeing 737 · Engine Exhaust System
  > PDA 3 #2 ENG PRIMARY EXH NOZZLE OUTBD SIDE FWD FENCE HAS ELONGATED HOLES IN NOZZLE ITSELF AND THE FENCE AND MISSING HI-LICK FASTENER. REMOVED AND REPLACED PRIMARY NOZZLE.
- [SDR CALA2022090202250](https://openairdocs.org/sdr/CALA2022090202250.md): Skin · broken · Sep 1, 2022 · N12218 · Boeing 737 · Fuselage Structure (General)
  > MRD BROKEN MRD *IAH 03-1402Z* FOR AIRCRAFT 0218 BROKEN ON 12AUG22 10:09:39 ON FLIGHT 1895 FROM IAH TO PHX. REASON: LOG PAGE 9288556 CREATE D NO FURTHER MAINTENANCE ACTION NEEDED
- [SDR CALA2021062500971](https://openairdocs.org/sdr/CALA2021062500971.md): Fitting · cracked · Jun 25, 2021 · N12218 · Boeing 737824 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT BS 540 RBL 6.14 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING IAW SRM 51-40-02, AMM 2-11-00, AND DWG 111A2000 REV ORIGINAL.
- [SDR CALA2021062500970](https://openairdocs.org/sdr/CALA2021062500970.md): Fitting · cracked · Jun 25, 2021 · N12218 · Boeing 737824 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT BS 540 RBL 32.40 IS CRACKED. REMOVED AND REPPLACED SHEAR FITTING IAW SRM 51-40-02 B7 37 NG, AMM 28-11-00, AND DWG 111A2000 REV ORIGINAL.
- [SDR CALA2021062500968](https://openairdocs.org/sdr/CALA2021062500968.md): Fitting · cracked · Jun 25, 2021 · N12218 · Boeing 737824 · Fuselage Main, Attach Fittings
  > SHEAR FITTING AT STA 540 LBL 32.40 IS CRACKED REMOVED AND REPLACED SHEAR FITTING IAW B737-800 SRM 51-40-02 AND B737 NG AMM 28-11-00 AND BAC DWG 111A2000 REV MORIGINAL.
- [SDR CALA2021062500967](https://openairdocs.org/sdr/CALA2021062500967.md): Fitting · cracked · Jun 25, 2021 · N12218 · Boeing 737824 · Fuselage Main, Attach Fittings
  > B737-57-4-1262 SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING IAW B737-800 SRM 51-40-02 B73 7 NG AMM 28-11-00 AND BAC DWG 111A2000 REV ORIGINAL.SEE NSA EMX N/R 00100 AND HANGER N/R 6227446. DATA WAS TRANSCRIBED FROM NSA EMX
- [SDR CALA2021062500965](https://openairdocs.org/sdr/CALA2021062500965.md): Fitting · cracked · Jun 25, 2021 · N12218 · Boeing 737824 · Fuselage Main, Attach Fittings
  > B737-57-4-1262 SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED REMOVED AND REPLACED SHEAR FITTING IAW B737-800 SRM 51-40-02 AND B737 NG AMM 28-11-00 AND BAC DWG 111A2000 REV ORIGINAL.SEE NSA EMX N/R 00105 AND HANGER N/R 6227451/DATA WAS TRANSCRIBED FROM N SA EMX
- [SDR CALA2021062500964](https://openairdocs.org/sdr/CALA2021062500964.md): Fitting · cracked · Jun 25, 2021 · N12218 · Boeing 737824 · Fuselage Main, Attach Fittings
  > B737-57-4-1262 SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING IAW B737-800 SRM 51-40-02 AND B737 NG AMM 28-11-00 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R 00103 AND HANGER N/R 6227449.DATA WAS TRANSCRIBED FROM N SA EM
- [SDR CALA2021062300939](https://openairdocs.org/sdr/CALA2021062300939.md): Fitting · cracked · Jun 22, 2021 · N12218 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED REMOVED AND REPLACED SHEAR FITTING IAW B737-800 SRM 51-40-02 B73 7 AMM 28-11-00 BAC DWG 111A-2000 REV ORIGINAL.
- [SDR CALA2021062300934](https://openairdocs.org/sdr/CALA2021062300934.md): Fitting · cracked · Jun 22, 2021 · N12218 · Boeing 737824 · Fuselage Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED REMOVED AND REPLACED SHEAR FITTING IAW B737-800 SRM 51-40-02 AND B737 NG AMM 28-11-00 AND BACDWG 111A2000 REV ORIGINAL,
- [SDR CALA2021062300933](https://openairdocs.org/sdr/CALA2021062300933.md): Fitting · cracked · Jun 22, 2021 · N12218 · Boeing 737824 · Fuselage Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED REMOVED AND REPLACED SHEAR FITTING IAW B737-800 SRM 51-40-02 AND B737 NG AMM 28-11-00 AND BAC DWG 111A2000 REV ORIGINAL,
- [SDR CALA2021062300932](https://openairdocs.org/sdr/CALA2021062300932.md): Fitting · cracked · Jun 22, 2021 · N12218 · Boeing 737824 · Fuselage Miscellaneous Structure
  > SHEAR FITTING AT STA 540 LBL 54.60 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING IAW B737-800 SRM 51-40-02 AND B737 NG AMM 28-11-00 AND BAC DWG 111A2000 REV ORIGINAL
- [SDR CALA2021062300935](https://openairdocs.org/sdr/CALA2021062300935.md): Fitting · cracked · Jun 22, 2021 · N12218 · Boeing 737824 · Fuselage Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED
- [SDR CALA2021062300931](https://openairdocs.org/sdr/CALA2021062300931.md): Fitting · cracked · Jun 22, 2021 · N12218 · Boeing 737824 · Fuselage Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED.
- [SDR CALA2021062300930](https://openairdocs.org/sdr/CALA2021062300930.md): Fitting · cracked · Jun 22, 2021 · N12218 · Boeing 737824 · Fuselage Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED
- [SDR CALA2021062300937](https://openairdocs.org/sdr/CALA2021062300937.md): Fitting · cracked · Jun 22, 2021 · N12218 · Boeing 737824 · Fuselage Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STA 540 LBL 32.40 IS CRACKED
- [SDR CALA2021062300936](https://openairdocs.org/sdr/CALA2021062300936.md): Fitting · cracked · Jun 22, 2021 · N12218 · Boeing 737824 · Fuselage Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED.
- [SDR CALA2017081402683](https://openairdocs.org/sdr/CALA2017081402683.md): Motor · odor · Aug 14, 2017 · N12218 · Boeing 737824 · Communications System
  > BURNING ODOR AT ROWS 23-25, TV ANTENNA MOTOR ABOVE ROWS 23-25 DEACTIVATED NO ODOR, COLLARED ANTENNA BREAKER
- [SDR CALA2017072402362](https://openairdocs.org/sdr/CALA2017072402362.md): Lens · missing · Jul 24, 2017 · N12218 · Boeing 737824 · Emergency Lighting
  > ROW 2 EMERGENCY LIGHT LENS IS MISSING. INSTALLED ROW 2 EMERGENCY PROXIMITY LIGHT LENS IAW IFM 25-27-42.
- [SDR CALA2017042901196](https://openairdocs.org/sdr/CALA2017042901196.md): Beam · cracked · Apr 29, 2017 · N12218 · Boeing 737824 · Service Doors
  > R1 DOOR BEAM CRACKED. THE DOOR FRAME WAS REPAIRED IAW EC/RA 5210-02823.
- [SDR CALA2017031700605](https://openairdocs.org/sdr/CALA2017031700605.md): Skin · damaged · Mar 15, 2017 · N12218 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STAB LOWER SKIN AT HSS 101.90. INSTALLED A REPAIR DOUBLER IAW SRM 55-10-01, REPAIR 11.
- [SDR CALA2017031700604](https://openairdocs.org/sdr/CALA2017031700604.md): Skin · cracked · Mar 14, 2017 · N12218 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STABILIZER LOWER SKIN AT HSS 101. NINTY INCHES FROM TRAILING EDGE HAS A.25 INCH CRACK. VERIFIED CRACK USING HFEC PART 651-00-00 PROCEDURE 23. INSTALLED A REPAIR DOUBLER IAW SRM 55-10-01, REPAIR 11.
- [SDR CALA2017022600487](https://openairdocs.org/sdr/CALA2017022600487.md): Pressure Panel · cracked · Feb 26, 2017 · N12218 · Boeing 737824 · Fuselage Main, Bulkhead
  > CENTER WING BOX REAR SPAR VERTICAL PRESSURE WEB BETWEEN RBL 31.83 AND RBL 40.00 (WL 200.6 AND WL 192.0) FOUND CRACK AFTER HFEC INSPECTION. (MARKED) REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM 57-10-10 REPAIR 3 ALTERNATIVE 2.
- [SDR CALA2017022400458](https://openairdocs.org/sdr/CALA2017022400458.md): Structure · corroded · Feb 23, 2017 · N12218 · Boeing 737824 · Service Doors
  > R-2 DOOR CHORD HAS CORROSION MULTIPLE AREAS FROM STA 947.5 TO STA 995. INSTALLED NEW RT CHORD PER SRM 51-40-02. INSPECTED R-2 DOOR CHORD PER SRM 51-40-02. NO DISCREPANCIES NOTED.
- [SDR CALA2017022400457](https://openairdocs.org/sdr/CALA2017022400457.md): Structure · corroded · Feb 23, 2017 · N12218 · Boeing 737824 · Service Doors
  > L-2 DOOR CHORD HAS CORROSION MULTIPLE AREAS FROM STA 950 TO STA 986. INSTALLED NEW L2 DOOR INNER CHORD. REFERENCE SRM 51-40-02. INSPECTED L-2 DOOR CHORD PER SRM 51-40-02. NO DISCREPANCIES NOTED.
- [SDR CALA2017022400454](https://openairdocs.org/sdr/CALA2017022400454.md): Intercostal · corroded · Feb 22, 2017 · N12218 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT VERTICAL INTERCOSTAL AT STA 792.5 CORRODED BETWEEN INTERCOSTAL ASSY STR 23L - 24L. INSTALLED INTERCOSTAL IAW SRM 51-40-02. INSPECTED INTERCOSTAL INSTALLATION.
- [SDR CALA2017022400453](https://openairdocs.org/sdr/CALA2017022400453.md): Intercostal · corroded · Feb 22, 2017 · N12218 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT INTERCOSTAL ASSY CORRODED BETWEEN STA 787 - 807 AT STR 23L. INSTALLED INTERCOSTAL IAW SRM 51-40-02. INSPECTED INSTALLATION OF INTERCOSTAL.
- [SDR CALA2017022400452](https://openairdocs.org/sdr/CALA2017022400452.md): Intercostal · corroded · Feb 22, 2017 · N12218 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT INTERCOSTAL ASSY CORRODED BETWEEN STA 787 - 807 STR 22L. INSTALLED INTERCOSTAL IAW SRM 51-40-02. INSPECTED INTERCOSTAL INSTALLATION.

Next page: https://openairdocs.org/aircraft/N12218/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 = 'N12218' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N12218/reports

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