# Service difficulty reports: N38268

A list on [N38268](https://openairdocs.org/aircraft/N38268.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR CALA2026030314275](https://openairdocs.org/sdr/CALA2026030314275.md): Skin · cracked · Mar 2, 2026 · N38268 · Boeing 737824 · Wing, Plate/Skin
  > PERFORMING EA 5720-02922 REV A OP 001 FOUND FASTENER HOLES 1, 2, 3, 4, 5, 6, 7, 8, & 12 OUT OF LIMITS IAW SRM 57-41-01-2R-7. PERFORMED REPAIR ON ON LT WING LEADING EDGE UPPER SKIN PANEL, WORK WAW ACCOMPLISHED IAW SRM 57-41-01-2R-8, EO 260081, REV P1, 260081
- [SDR CALA2026010212599](https://openairdocs.org/sdr/CALA2026010212599.md): Battery Pack · inoperative · Dec 31, 2025 · N38268 · Boeing 737824 · Emergency Lighting
  > FOUND FIRST CLASS AND OVERWING EMERGENCY EXIT LIGHTS NOT TURNING ON. REMOVED AND REPLACED BATTERY PACKS M1674, M1675, AND M1695 IAW AMM 33-51-06-960-805 OPS CHECKED GOOD.
- [SDR CALA2025101309961](https://openairdocs.org/sdr/CALA2025101309961.md): Fuse · inoperative · Oct 10, 2025 · N38268 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK. LT EMERGENCY WING EXIT SEAT LIGHTS NOT WORKING (15, 20 & 21ABC) AND RT (20DEF) LOWER WING EMERGENCY EXIT SIGN NOT WORKING. RELAMPED ALL LIGHTS ON RT LOWER WING EMERGENCY EXIT SIGN ON ROW 20DEF IAW AMM: 33-51-01-960
- [SDR CALA2025090508488](https://openairdocs.org/sdr/CALA2025090508488.md): Stop Ring · broken · Sep 3, 2025 · N38268 · Boeing 737824 · Emergency Equipment
  > DOOR 1L LEFT SIDE GIRT BAR BRACKET BROKEN. LEFT PLASTIC STOP RING ON L1 SLIDE IS BROKEN. REMOVED AND REPLACED THE LEFT HAND PLASTIC BAR STOP LOCK ON L1 SLIDE REF AMM TASK 25-66-001-00-803/804. GIRT BAR LOCK AND SPRING PIN PROPERLY INSTALLED REF AMM 25-66-
- [SDR CALA2025031802922](https://openairdocs.org/sdr/CALA2025031802922.md): Slide · damaged · Mar 17, 2025 · N38268 · Boeing 737824 · Escape Slide
  > DOOR OPENED W/ SLIDE ATTACHED. DID NOT DEPLOY FLAGGING SDR EVENT REMOVE OLD SLIDE PACK FROM DOOR 1 LEFT AND INSTALLED A NEW SLIDE PACK REF AMM 25-66-01 ABSORBED REMOVAL & INSTALLATION OF L1 SLIDE PER AMM 25-66-01. & GMM 09-25-05 AND ESCAPE SLIDE RENDER SAFE CH
- [SDR CALA2025031702855](https://openairdocs.org/sdr/CALA2025031702855.md): Light · no test · Mar 12, 2025 · N38268 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - PROXIMITY LIGHT SEAT ROW 14ABC INOP R+R FLOOR PROXIMITY LIGHT ASSY IAW AMM 33-51-11 FAULT STILL OCCURS. TROUBLESHOOT USING FIM 33-50 TASK 801. FOUND WIRES DISCONNECTED UNDER SEAT. RE-CONNECTED IAW
- [SDR CALA2024111102814](https://openairdocs.org/sdr/CALA2024111102814.md): Battery Pack · inoperative · Nov 8, 2024 · N38268 · Boeing 737824 · Emergency Lighting
  > VARIOUS EMERGENCY LIGHTS IN THE CABIN DID NOT ILLUMINATE PROPERLY DURING TESTING. SUPPORT TASK NSA EMX N/R 00178. AIR GRILLES AT RIGHT HAND SEAT ROW 8 AND LEFT HADN SEAT ROW 15 IAW B737NG AMM 21-23-03-400-802. REMOVED RETURN AIR GRILLE AT RIGHT HAND SEAT ROW 2
- [SDR CALA2024070800162](https://openairdocs.org/sdr/CALA2024070800162.md): Sensor · faulty · Jul 6, 2024 · N38268 · Boeing 737824 · Air Distribution System
  > PASSING THRU 10000FT RT PACK LIGHT WITH CAUTION ILLUMINATED. RAN QRH PACK LIGHT REMAINS ON. CREW STATES RT PACK LIGHT CAME ON GOING THROUGH 10,000FT. CABIN WAS REALLY HOT SPECIALLY TOWARDS AFT OF ACFT. COCKPIT TEMP COMFORTABLE, AIR WAS WORKING AS NORMAL. THERE
- [SDR CALA2024062601900](https://openairdocs.org/sdr/CALA2024062601900.md): Battery Pack · no test · Jun 22, 2024 · N38268 · Boeing 737824 · Emergency Lighting
  > EMERGENCY BATTERY PACK M1676 FAILS CAPACITY CHECK.
- [SDR CALA2024062101880](https://openairdocs.org/sdr/CALA2024062101880.md): Skin · cracked · Jun 21, 2024 · N38268 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RH HORIZONTAL STABILIZER, LOWER SKIN STAB STA 157.10, 10.5 INCHE S FORWARD TO TRAILING EDGE HAS CRAK INDICATION (REF. AAR NR 1000 12424)
- [SDR CALA2024062001876](https://openairdocs.org/sdr/CALA2024062001876.md): Skin · deformed · Jun 17, 2024 · N38268 · Boeing 737824 · Cargo/Baggage Doors
  > RE-SKIN AFT CARGO DOOR.
- [SDR CALA2024021200386](https://openairdocs.org/sdr/CALA2024021200386.md): Angle · worn · Jan 31, 2024 · N38268 · Boeing 737824 · Fuselage Main, Bulkhead
  > L/H WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE CRACKED APPROXIAMATELY AT LBL 9.0.SUPPORT TASK NSA EMX N/R 00128.: REMOVED THE DAMAGED SECTION OF ATTACH ANGLE AL L/H WING TRANSCRIBED FROM NSA EMX N/R 00128. WORK ACCOMPLISHED BY CENTER SECTION RE
- [SDR CALA2024021300408](https://openairdocs.org/sdr/CALA2024021300408.md): Fitting · cracked · Jan 25, 2024 · N38268 · Boeing 737824 · Fuselage Main, Attach Fittings
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00111. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 ACCOMPLISHED BY V905004 AND INSPECTED BY V895775. SSFR REPORT FORM 46-0024, ENTERED BY UAL INS
- [SDR CALA2024021200382](https://openairdocs.org/sdr/CALA2024021200382.md): Fitting · cracked · Jan 25, 2024 · N38268 · Boeing 737824 · Fuselage Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED.SUPPORT TASK NSA EMX N/R 00110. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL
- [SDR CALA2024021200381](https://openairdocs.org/sdr/CALA2024021200381.md): Fitting · cracked · Jan 25, 2024 · N38268 · Boeing 737824 · Fuselage Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 6. 14 IS CRACKED. SUPPORT TASK NSA EMX N/R 00113 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL N/R 00113. IAW-800 SRM 51-40--02 AND BAC DWG 111A2000 REV
- [SDR CALA2024021200380](https://openairdocs.org/sdr/CALA2024021200380.md): Fitting · cracked · Jan 25, 2024 · N38268 · Boeing 737824 · Fuselage Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00115 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 32.40 IAW B737-800 SRM 51--40-02 AND BAC DWG# 111A2000 REV ORIGINAL SSFR REPORT FORM 46-0024,
- [SDR CALA2024021200379](https://openairdocs.org/sdr/CALA2024021200379.md): Fitting · cracked · Jan 25, 2024 · N38268 · Boeing 737824 · Fuselage Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED.SUPPORT TASK NSA EMX N/R 00112. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL N/R 00112 32.40 IAW B737-800 SRM 51-40-02 AND BAC DWG# 111A2000 REV SSFR REPORT FORM 46-0024, ENTERED
- [SDR CALA2024021200378](https://openairdocs.org/sdr/CALA2024021200378.md): Fitting · cracked · Jan 25, 2024 · N38268 · Boeing 737824 · Wing Miscellaneous Structure
  > B737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00114 REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 15.04 IAW B737-800 SRM 51--40-02 AND BAC DWG #111A2000 REV ORIGINAL SSFR REPORT FORM 46-0024, ENTERED
- [SDR CALA2023122103705](https://openairdocs.org/sdr/CALA2023122103705.md): Unknown · unknown · Dec 18, 2023 · N38268 · Boeing 737824 · Central Warning
  > REJECTED TAKEOFF AT 120 KNOTS FOR WINDSHEAR WARNING. AS PER INFORMATION FROM CREW - REJECTED TAKE OFF GROSS WEIGHT 153.3K LBS AT 120KIAS PERFORMED PHASE 1A INSPECTION PER AMM 05-51-01 NO DAMAGE FOUND A/C OK TO CONT.
- [SDR CALA2022052501338](https://openairdocs.org/sdr/CALA2022052501338.md): Anti-Skid Valve · faulty · May 25, 2022 · N38268 · Boeing 737924ER · Brake
  > *EMERGENCY DECLARED* ANTISKID INOP LIGHT LIGHT ON BITE TEST SHOWS VALVE 1 FAULTED. APPLY MEL 3202C FOR ANTISKID P6-3 PULLED AND COLLARED. OUTBOARD CHANNEL. OUTBOARD CHANNEL INOP. COMPLIED WITH DDPG. CIRCUIT BREAKER AT MEL 3202C UABLE AIRCRAFT ARRIVED TO GATE W
- [SDR CALA2022042501075](https://openairdocs.org/sdr/CALA2022042501075.md): Stabilizer · inoperative · Apr 25, 2022 · N38268 · Boeing 737824 · Stabilizer Position Indicating
  > *EMERGENCY DECLAERD* NO TRIM ON EITHER SIDE USED CAPT ATHORITY PULLED BREAKER ONCE NO JOY LOCKING UNLOCKING REPLACED STAB TRIM MOTOR. REF MM 27-41-71-400-801. COMPLETED PERFORMED STAB TRIM MOTOR AUTOPILOT TEST PER AMM 22-11-81; TEST STAB TRIM LIMIT SWITCH TES
- [SDR CALA2022042101033](https://openairdocs.org/sdr/CALA2022042101033.md): Window Frame · cracked · Apr 20, 2022 · N38268 · Boeing 737824 · Fuselage Main, Frame
  > INITIATE A DTA DIP FOR THE R1 WINDOW FRAME REPAIR TO ?ACCOMPLISH AN INITIAL INSPECTION PER PART 2, SECTION B ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL AIRCRAFT FLIGHT CYCLES. ACCOMPLISH REPETITIVE INSPECTIONS PER PART 2, SECTION B AT INTERVALS NOT TO EX
- [SDR CALA2022042101032](https://openairdocs.org/sdr/CALA2022042101032.md): Window Frame · cracked · Apr 19, 2022 · N38268 · Boeing 737824 · Fuselage Main, Frame
  > INITIATE A DTA DIP FOR THE L1 WINDOW FRAME REPAIR TO ?ACCOMPLISH AN INITIAL INSPECTION PER PART 2, SECTION B ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL AIRCRAFT FLIGHT CYCLES. ACCOMPLISH REPETITIVE INSPECTIONS PER PART 2, SECTION B AT INTERVALS NOT TO EXC
- [SDR CALA2022041100949](https://openairdocs.org/sdr/CALA2022041100949.md): Skin · cracked · Apr 9, 2022 · N38268 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HAND HORIZONTAL STAB LOWER SKIN AREA STA. 147.90, 10 INCH ES FROM TRAILING EDGE SPAR CRACK INDICATION NOTED, REFENCE FLEET CYCLE LOG 9805813. TO INSPECT DVI AND LFEC AT 56000 TOTAL FLIGHT CYCLES AND DVI AND LFEC EVERY 9000 THERE AFTER. PER FIGURE 206OF
- [SDR CALA2022041100948](https://openairdocs.org/sdr/CALA2022041100948.md): Skin · cracked · Apr 9, 2022 · N38268 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HAND HORIZONTAL STAB LOWER SKIN AREA STA. 101.90, 12 INCH FROM FRONT SPAR CRACK INDICATION NOTED, REFERENCE FLEETCYCLE 9805811. TO INSPECT DVI AND LFEC AT 56000 TOTAL FLIGHT CYCLES AND DVI AND PER FIGURE 206 OF SRM 55-10-01-2R-11. LFEC EVERY 9000 THERE A
- [SDR CALA2022033100834](https://openairdocs.org/sdr/CALA2022033100834.md): None · none · Mar 30, 2022 · N38268 · Boeing 7378 · Wing, Center Box
  > INSPECTION (HFEC) OF THE RIGHT WHEEL WELL CENTER WING BOX REAR SPAR VERTICAL WEB, CRACK NOTED INBD OF RBL45.64. TABLE 205. INITIAL INSPECTION REQUIRED 56,000 FLIGHT CYCLES AND THEREAFTER, INTERVAL 36,000 FLIGHT CYCLES. REPAIRED PER SRM ON FLEET CYCLE LP 98069
- [SDR CALA2021030500258](https://openairdocs.org/sdr/CALA2021030500258.md): Pump · defective · Mar 4, 2021 · N38268 · Boeing 737824 · Hydraulic Pump (Electric/Engine), Main
  > ENG 2 LOW PRESSURE LIGHT LIGHT ON LIGHT ILLUMINATED ON CLIMB OUT. UPON ARRIVAL FOUND #2 ENGINE DRIVEN HYDRAULIC PUMP PAD DRAIN LEAKING. B HYDRAULIC SYSTEM FOUND TO BE EMPTY AND STBY SYSTEM LOW QTY LIGHT ILLUMINATED. #2 ENGINE OIL SAMPLES TAKEN AFTER ARRIVAL. R
- [SDR CALA2017112504210](https://openairdocs.org/sdr/CALA2017112504210.md): Lens · missing · Nov 25, 2017 · N38268 · Boeing 737824 · Emergency Lighting
  > SEAT 15C AFT AISLE EMERGENCY LIGHT LENS IS MISSING EPL LENS MISSING IS THE RED AT ROW 15C. LIGHT IS STILL OPERATION AL AT THIS TIME. INSTALLED NEW RED EPL LENS AT SEAT 15C PER VMM 25-22-55. NO FURTHER DEFECTS.
- [SDR CALA2017100603528](https://openairdocs.org/sdr/CALA2017100603528.md): Sign · damaged · Oct 6, 2017 · N38268 · Boeing 737824 · Emergency Lighting
  > EMERGENCY EXIT SIGN ABOVE 20A DAMAGED. ON REMOVAL FOUND FWD MOUNT AND ENTIRE SEAL RETAINER ASSEMBLY DEBONDED FROM THE PANEL. ACCOMPLISHED A REPAIR IAW AMM 25-00-00, GPM 01-08-024 AND DRAWING 411A2810-3.
- [SDR CALA2017051501456](https://openairdocs.org/sdr/CALA2017051501456.md): Slide · unserviceable · May 15, 2017 · N38268 · Boeing 737824 · Escape Slide
  > 2L MED ESCAPE SLIDE PRESSURE IS BELOW LIMITS. REPLACED ESCAPE SLIDE REF AMM25-66-01-400-801.
- [SDR CALA2016032900194](https://openairdocs.org/sdr/CALA2016032900194.md): Skin · cracked · Mar 29, 2016 · N38268 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STABILIZER, LOWER INSPAR SKIN HAS A CRACK, AT STAB STATION 129.5, 34" AFT OF THE LE SPAR. INSTALLED REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11.
- [SDR CALA2016032800192](https://openairdocs.org/sdr/CALA2016032800192.md): Skin · cracked · Mar 28, 2016 · N38268 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL LOWER INSPAR SKIN HAS A CRACK AT STAB STATION 147.9 8, 5" AFT OF LE SPAR. INSTALLED REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11.
- [SDR CALA2016032800188](https://openairdocs.org/sdr/CALA2016032800188.md): Beam · cracked · Mar 26, 2016 · N38268 · Boeing 737824 · Passenger/Crew Doors
  > PLEASE COMPLY WITH ECRA 5210-02705. ACFT 0268, R1 DOOR BEAM CRACK INSPECTION & REPAIR R & R R1 DOOR LOWER DOOR BEAM IAW SRM 51-40-02 & DWG 141A6516.
- [SDR CALA2016032800187](https://openairdocs.org/sdr/CALA2016032800187.md): Skin · dented · Mar 25, 2016 · N38268 · Boeing 737824 · Fuselage Main, Plate/Skin
  > DENT IN RT FWD FUSELAGE, 14" FWD OF GND POWER RECEPTACLE CUT OUT, AT STATION 215. REPAIRED DENT IAW SRM 53-00-01 REPAIR 3.
- [SDR CALA2012120300828](https://openairdocs.org/sdr/CALA2012120300828.md): Power Supply · inoperative · Dec 3, 2012 · N38268 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS AT SEATS 8C THROUGH 12C INOPERATIVE. FOUND EMERGENCY LIGHT AT 8C SHORTED. DISCONNECTED LIGHT ASSY AND TAPED CONNECTOR. REPLACED BATTERY CHARGER IN SIDEWALL AT 8ABC. LIGHTS AT 9C THRU 12C, OPS NORMAL. IDT 172337 CR NO PARTS AVAILABLE MEL
- [SDR CALA2012092600627](https://openairdocs.org/sdr/CALA2012092600627.md): Charger · inoperative · Sep 26, 2012 · N38268 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHTS ON SEATS 8 THRU 12 INOPERATIVE. FOUND FAULTY BATTERY CHARGER AT POSITION M1676. R & R BATTERY CHARGER REF MM 33-51-06. OPS CHECKED NORMAL.
- [SDR CALA2012082900552](https://openairdocs.org/sdr/CALA2012082900552.md): Electronic Unit · failed · Aug 25, 2012 · N38268 · Boeing 737824 · Navigation System
  > AT 39000 FT DISPLAY SOURCE LIGHT CAME ON. LOST HYD SYS A INDICATION, CAPTAIN`S SPEED LIM IND-LOSS OF SPEED BANDS-WX RANGE DISAGREE.1.5 MIN, FOLLOWED BY DISPLAY SOURCE CHECKLIST. LOST F/D AT 1000FT ON APPROACH. CDS FAULT ON GROUND. NO CB OUT. R & R /31 DEU
- [SDR CALA2012041800276](https://openairdocs.org/sdr/CALA2012041800276.md): Sign · broken · Apr 18, 2012 · N38268 · Boeing 737824 · Emergency Lighting
  > THE EXIT SIGN AT SEAT 21F FELL OFF. REMOVED AND REPLACED EMER EXIST SIGN ASSY AT 21F AS PER 33-50-0 0. OPS CHECKS GOOD.
- [SDR CALA2011071800499](https://openairdocs.org/sdr/CALA2011071800499.md): Skin · damaged · Jul 18, 2011 · N38268 · Boeing 737824 · Cargo/Baggage Doors
  > SUPPORT TASK - THE C2 DOOR HAS 2 CREASES SIDE BY SIDE 32 INCHES FROM THE BOTTOM EDGE OF THE DOOR, AND 16 AND 19 INCHES FROM THE FWD EDGE. REPAIRED C2 DOOR REF SRM 52-00-01 REPAIR 3.
- [SDR CALA2011071500494](https://openairdocs.org/sdr/CALA2011071500494.md): Skin · cracked · Jul 15, 2011 · N38268 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > SUPPORT TASK RT HORIZONTAL STAB LOWER SKIN HAS CRACKED AT SS 13 8.70. INSTALLED REPAIR REF:SRM 55-10-01 REPAIR 11.
- [SDR CALA2011071100480](https://openairdocs.org/sdr/CALA2011071100480.md): Floorbeam · corroded · Jul 10, 2011 · N38268 · Boeing 737824 · Fuselage Main, Floor Beam
  > STA 986.5 FLOORBEAM HAS CORR AT FASTENER HOLE LBL 43. REPAIRED CABIN FLOORBEAM STA 986.5 LBL 43 PER ECRA 5321-01429 ATTACH FORM 44.0008,PAGE 1 TO PAGE 2- ITEM 1 TO ITEM 12.
- [SDR CALA2011071100479](https://openairdocs.org/sdr/CALA2011071100479.md): Floorbeam · corroded · Jul 10, 2011 · N38268 · Boeing 737824 · Fuselage Main, Floor Beam
  > STA 986.5 FLOORBEAM HAS CORR AT FASTENER HOLE RBL 43 REPAIRED CABIN FLOORBEAM STA 986.5 RBL 43 PER ECRA 5321-01429 ATTACHED FORM 44.0008 PAGE 1 TO PAGE 2, ITEM 1 TO ITEM 10.
- [SDR CALA2011070700466](https://openairdocs.org/sdr/CALA2011070700466.md): Frame · cracked · Jul 7, 2011 · N38268 · Boeing 737824 · Fuselage Main, Frame
  > SUPPORT TASK PAX CABIN HAS CRACKED FRAME 500FL BETWEEN STR 9L AND 8L. REPAIRED CRACKED FRAME AT STA 500F LEFT SIDE. REF EA 5310-04716 REV C OPS 2.
- [SDR CALA2011070700463](https://openairdocs.org/sdr/CALA2011070700463.md): Frame · cracked · Jul 6, 2011 · N38268 · Boeing 737824 · Fuselage Main, Frame
  > PASSENGER CABIN, RT SIDEWALL,STA 480 & S-8R. FRAME APPEARS TO BE CRACKED AT I/B FASTENER WHERE PSU BRACKET ASSEMBLY ATTACHES TO FRAME (MARKED). REPAIRED CRACKED FRAME PER EA5310-04716 REV C OP02.
- [SDR CALA2011070700464](https://openairdocs.org/sdr/CALA2011070700464.md): Frame · cracked · Jul 6, 2011 · N38268 · Boeing 737824 · Fuselage Main, Frame
  > SUPPORT TASK STA 400R HAS CRACKED FRAME BETWEEN STR8-9 AT PSU ATTACH BRACKET. REPAIRED PER EA 5310-04716 REV C.
- [SDR CALA2011070700465](https://openairdocs.org/sdr/CALA2011070700465.md): Frame · cracked · Jul 6, 2011 · N38268 · Boeing 737824 · Fuselage Main, Frame
  > SUPPORT TASK - STA 380R HAS CRACKED FRAME BETWEEN STR 8-9 PSU AT TACH BRACKET. REPAIRED FRAME STA 380R, STR 8-9 PER EA 5310-04716 REV C.
- [SDR CALA2011070700462](https://openairdocs.org/sdr/CALA2011070700462.md): Intercostal · cracked · Jul 6, 2011 · N38268 · Boeing 737824 · Fuselage Miscellaneous Structure
  > CABIN FLOOR INTERCOSTAL CRACKED AT BL 0 STA 344-360. INSTALLED NEW INTERCOSTALL REF SRM 51-40-02.
- [SDR CALA2011021100083](https://openairdocs.org/sdr/CALA2011021100083.md): Light · inoperative · Feb 11, 2011 · N38268 · Boeing 737824 · Emergency Lighting
  > RT OVERWING AFT EMERGENCY LIGHT INOP. REPLACED RT OVERWING AFT EMERGENCY LIGHT, OPS CHECKS GOOD.

## 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 = 'N38268' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N38268/reports

---
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.