# Service difficulty reports: N34282

A list on [N34282](https://openairdocs.org/aircraft/N34282.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 · 78 reports

- [SDR CALA2026011913078](https://openairdocs.org/sdr/CALA2026011913078.md): None · no discrepancy · Jan 18, 2026 · N34282 · Boeing 737824 · Cabin Equipment/Furnishings
  > PLASTIC ODOR IN PLANE, SMELLS LIKE NEW INTERIOR, NO SMOKE ODOR NOTED. OKAY FOR SERVICE AT THIS TIME IAW AMM 05-51-26-800-801-C1.
- [SDR CALA2026011913065](https://openairdocs.org/sdr/CALA2026011913065.md): Attach Angle · cracked · Jan 16, 2026 · N34282 · Boeing 737824 · Fuselage Main, Attach Fittings
  > RIGHT BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT APPROX RBL 9.0. SUPPORT TASK NSA EMX N/R 00061. REPAIRED UPPER ATTACH ANGLE AT BS 663 BULKHEAD VAPOR BARRIER RBL 9.0 IAW SRM 57-10-10-2R-5, REPAIR 5.
- [SDR CALA2026011412954](https://openairdocs.org/sdr/CALA2026011412954.md): Shear Fitting · cracked · Jan 8, 2026 · N34282 · Boeing 737824 · Fuselage Main, Structure
  > SHEAR FITTING AT BS 540 AND LBL 6.14 IS CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02 AND DWG 111A2000 REV ORIGINAL.
- [SDR CALA2026011412952](https://openairdocs.org/sdr/CALA2026011412952.md): Shear Fitting · cracked · Jan 8, 2026 · N34282 · Boeing 737824 · Fuselage Main, Structure
  > SHEAR FITTING AT BS 540, RBL 15.04 CRACKED. R & R THE SHEAR FITTING IAW SRM 51-40-02, & DWG 111A2000, REV ORIGINAL.
- [SDR CALA2025102410497](https://openairdocs.org/sdr/CALA2025102410497.md): Lens · detached · Oct 23, 2025 · N34282 · Boeing 737824 · Emergency Lighting
  > FWD RIGHT DOOR EMRGNCY EXIT SIGN DETACHED FROM HOUSING RESECURED LENS COVER. OPS CHECK OF DOOR 1R EMERGENCY LIGHTS GOOD REF AMM 33-51-01-960-802.
- [SDR CALA2025081507850](https://openairdocs.org/sdr/CALA2025081507850.md): Light · inoperative · Aug 13, 2025 · N34282 · Boeing 737824 · Emergency Lighting
  > FA REPORTS 20C SIDE SEAT EMER LIGHT INOPERATIVE. SWAPPED LIGHT FROM 20C WITH 14C IAW AMM 33-51-11, OPS CHECKS ON 20C OK, DEFERRED 14C FLOOR ESCAPE PATH LIGHT IAW MEL 3319E.
- [SDR CALA2025051204608](https://openairdocs.org/sdr/CALA2025051204608.md): Elec Connector · mispinned · May 9, 2025 · N34282 · Boeing 737824 · Light System Wiring
  > RH FWD OVERWING INTERIOR EMERGENCY EXIT DOOR LIGHT INOP R/R M1695 EMERGENCY BATTERY CHARGER IAW AMM 33-51-06. NO HELP. FOUND D12456P PINNED INCORRECTLY REF WDM 33-51-13A SHEET 3 DETAIL A. REPLACED WITH HARNESS FROM ROBBED ASSY. REPLACED LIGHT ASSEMBLY, OPS CH
- [SDR CALA2025021102289](https://openairdocs.org/sdr/CALA2025021102289.md): Slide · out of adjust · Feb 8, 2025 · N34282 · Boeing 737824 · Escape Slide
  > DOOR 1R FA REPORTS THE GIRT BAR IS VERY HARD TO INSERT INTO ITS BRACKET ON THE DOOR. ADJUSTED/TUCKED Z FOLD OF ESCAPE SLIDE MATERIAL IAW AMM TASK 25-66-01-400-804. GIRT BAR STOWES NORMALLY IN SLIDE PACK BRACKETS.
- [SDR CALA2025012802091](https://openairdocs.org/sdr/CALA2025012802091.md): Windshield · cracked · Jan 27, 2025 · N34282 · Boeing 737824 · Flight Compartment Windows
  > R2 WINDOW OVERHEAT ELEC SPARKS OBSERVED OUTSIDE WINDOW...QRH PRO C DID NOT CORRECT PRB ADDED SDR REPORT AND PICTURES PARTS USED: 29-5612-9-9006,QTY:1 29-3041-9-0002,QTY:1 29-3040-3-0006,QTY:1 141A4810-116CAL,QTY:1 REPLACED R2 OPENABLE WINDOW REF AMM 56-
- [SDR CALA2025011500119](https://openairdocs.org/sdr/CALA2025011500119.md): Battery Pack · discharged · Jan 13, 2025 · N34282 · Boeing 737824 · Emergency Lighting
  > EMERGENCY BATTERY PACK M1672 DOES NOT CHARGE. REMOVED AND INSTALLED NEW EMERGENCY BATTERY PACK POS M1672 IAW AMM 33-51-06-960-805, OPERATIONAL TESTED GOOD.
- [SDR CALA2025010700052](https://openairdocs.org/sdr/CALA2025010700052.md): Structure · corroded · Dec 24, 2024 · N34282 · Boeing 737824 · Wing Main, Frame Structure
  > RH WING DRY BAY WS 736.50 AREA HAS CORROSION.(REF AAR NR 1000025 375) REPAIRED RH WING DRY BAY WS 736.50 ALL WORK DONE IAW B737-800 ECRA 240671 REV P1 AND IR.
- [SDR CALA2024121803104](https://openairdocs.org/sdr/CALA2024121803104.md): Skin · damaged · Dec 11, 2024 · N34282 · Boeing 737824 · Cargo/Baggage Doors
  > RESKIN AFT CARGO DOOR. REMOVED AND REPLACED AFT CARGO DOOR SKIN IAW B737 SRM 51-40-02-0 G-0, SRM 51-40-08-0G-0,SRM 51-20-01-0G-0,AMM51-21-72-370-803,SRM 52-30-01-2R-3, AMM 51-21-99-300 AND DRW 143A6112 AND 143A6110.
- [SDR CALA2024121803101](https://openairdocs.org/sdr/CALA2024121803101.md): Skin · damaged · Dec 11, 2024 · N34282 · Boeing 737824 · Cargo/Baggage Doors
  > RESKIN FWD CARGO DOOR (REF. AAR NR 1000021053) REMOVED AND REPLACED FWD CARGO DOOR EXTERNAL SKIN IAW B737 SRM 5 937984. 1-40-02-0G-0, SRM 51-40-05-0G-0,SRM 51-40-08-0G-0,SRM 51-20-01-0 G-0,AMM 51-21-72-370-803,SRM 52-30-01-2R-3,AMM 51-21-99-300 AND DRW 143A61
- [SDR CALA2024100100739](https://openairdocs.org/sdr/CALA2024100100739.md): Filter · dirty · Sep 29, 2024 · N34282 · Boeing 737824 · Air Conditioning System
  > FUMES OR SMOKE IN CABIN PNEUMATIC POWER SUPPLIED BY ENGINE ENGIN E 1 STRONG FUME SMELL WAS NOTICED IN THE FLIGHT DECK ON TAKE OFF AND INITIAL CLIMB TOMC LOCKING LOG PAGE TO ACCOMPLISH FIM SMOKE OR FUMES IN THE CABIN, SOURCE UNKNOWN - FAULT ISOLATION 21-00 TAS
- [SDR CALA2024091000615](https://openairdocs.org/sdr/CALA2024091000615.md): Indicator · faulted · Sep 7, 2024 · N34282 · Boeing 737824 · Airspeed/Mach Indicator
  > IAS DISAGREE AT FL380 RAN QRC QRH. RESULTED IN A RETURN TO GUM. CAPT SI DE WAS 15 KTS SPLIT. FLUSHED AND DEBRIS REMOVED FROM LEFT (CAPT'S) PITOT PROBE REF AMM 34-11-00-170-802 (ALTERNATE METHOD). PERFORMED LEFT PITOT LEAK TEST REF AMM 34-11-00-790-810. LEAK TE
- [SDR CALA2024090902403](https://openairdocs.org/sdr/CALA2024090902403.md): Warning Message · false activation · Sep 7, 2024 · N34282 · Boeing 737824 · Central Warning
  > IAS DISAGREE AT FL380 RAN QRC QRH. RESULTED IN A RETURN TO GUM. CAPT SI DE WAS 15 KTS SPLIT. FLUSHED AND DEBRIS REMOVED FROM LEFT (CAPT''S) PITOT PROBE REF GOOD. -END- AMM 34-11-00-170-802 (ALTERNATE METHOD). PERFORMED LEFT PITOT LEAK TEST REF AMM 34-11-00-790
- [SDR CALA2024061901863](https://openairdocs.org/sdr/CALA2024061901863.md): Motor · faulted · Jun 19, 2024 · N34282 · Boeing 737824 · Flight Control System
  > TRIM SWITCH DOES NOT OPERATE CORRECTLY ELEC TRIM INOP BOTH LEFT AND RIGT YOKE. UP AND DOWN INOP. REMOVED AND REPLACED STAB TRIM MOTOR IAW AMM 27-41-71 OP CHECK GOOD IAW AMM 27-41-71, 27-41-00, AND 22-11-81.
- [SDR CALA2022122803515](https://openairdocs.org/sdr/CALA2022122803515.md): Warning Light · false activation · Dec 28, 2022 · N34282 · Boeing 737824 · Flight Control System
  > FEEL DIFF PRESS LIGHT LIGHT ON ON APPROX 300FEET AFTER TAKEOFF. OFF SOMETIME AFTER LANDING BEFO RE BLOCKIN PERFORMED FIM 27-31 TASK 815, FOUND BOTH LEFT AND RIGHT RESTRICTOR VALVES CLOGGED. CLEANED AND RE-INSTALLED BOTH. PERFORMED OPERATIONAL AND LEAK CHECKS W
- [SDR CALA2021092801705](https://openairdocs.org/sdr/CALA2021092801705.md): Skin · none · Sep 28, 2021 · N34282 · Boeing 737824 · Fuselage Main, Plate/Skin
  > A REPAIR DOUBLER WAS INSTALLED ON LEFT SIDE FUSELAGE STATION 177.73 TO 259.45 STRINGER 24L WHICH REQUIRES AN INITIAL INSPECTION. ACCOMPLISH INITIAL INSPECTIONS PER PART 2 OF LATEST REVISION OF EC 5331-02644 ON OR BEFORE THE AIRCRAFT REACHES 50,000 TOTAL FLIGH
- [SDR CALA2021092801701](https://openairdocs.org/sdr/CALA2021092801701.md): Skin · cracked · Sep 27, 2021 · N34282 · Boeing 737824 · Empennage Structure
  > SUPPORT TASK EA 5510-01843 OP1 LH HORIZONTAL STABILIZER LOWER IN- SPAR SKIN PANEL FOUND CRACK AT STA 157.1 DETAILS REFER ATTACHED FIG. TRANSSFER REF NON- ROUTINE L/P 9130285 AND ORIGINA TED BY V897399 9,000 FLIGHT CYCLES THEREAFTER. CREATED DIP TO ACCOMPLISH S
- [SDR CALA2021092801700](https://openairdocs.org/sdr/CALA2021092801700.md): Skin · cracked · Sep 27, 2021 · N34282 · Boeing 737824 · Empennage Structure
  > SUPPORT TASK EA 5510-01843 OP1 LH HORIZONTAL STABILIZER LOWER IN- SPAR SKIN PANEL FOUND CRACK BETWEEN STA 92.7 AND 101.9 DETAIL REFER ATTACHED FIG. TRANSFER REF NON- ROUTINE L/P 9130286 AND ORIGINATED BY V897399 9,000 FLIGHT CYCLES THEREAFTER. CREATED DIP TO A
- [SDR CALA2021092801704](https://openairdocs.org/sdr/CALA2021092801704.md): Skin · cracked · Sep 27, 2021 · N34282 · Boeing 737824 · Doors
  > INSPECT EVERY 1500 FLIGHT HOURS OR MORE FREQUENTLY PERFORM PERM ANENT REPAIR 2C CHECK 04-07-2016 REF SRM 52-30-01 AD1 PG 105 AN D LOG PAGES8137215 AND 4693771 DENT IN AFT CARGO DOOR 18" FROM TOP AND 14" FROM FWD EDGE 3.75 X 4.5 DEPTH.197 SC CK LIMITS 12,500 H
- [SDR CALA2021092801702](https://openairdocs.org/sdr/CALA2021092801702.md): Skin · cracked · Sep 27, 2021 · N34282 · Boeing 737824 · Empennage Structure
  > SUPPORT TASK EA 5510-01843 OP 1 LH HORIZONTAL STABILIZER LOWER IN- SPAR SKIN PANEL FOUND CRACK AR STA 120.3 DETAILS REFER ATTACHED FIG. TRANSFER REF NON- ROUTINE L/P 9130284 AND ORIGINAT ED BY V897399 INSPECTIONS AT 9,000 FLIGHT CYCLES THEREAFTER. CREATED DIP
- [SDR CALA2021092701698](https://openairdocs.org/sdr/CALA2021092701698.md): Panel · cracked · Sep 27, 2021 · N34282 · Boeing 7378 · Empennage Structure
  > SUPPORT TASK EA 5510-01843 OP1 LH HORIZONTAL STABILIZER LOWER IN- SPAR SKIN PANEL FOUND CRACK BETWEEN STA 92.7 AND 101.9 DETAIL REFER ATTACHED FIG. TRANSFER REF NON- ROUTINE L/P 9130286 AND ORIGINATED BY V897399 THIS ITEM WAS REPAIRED IAW SRM 55-10-01-2R-11 RE
- [SDR CALA2021092701690](https://openairdocs.org/sdr/CALA2021092701690.md): Panel · cracked · Sep 27, 2021 · N34282 · Boeing 7378 · Empennage Structure
  > SUPPORT TASK EA 5510-01843 OP 1 LH HORIZONTAL STABILIZER LOWER IN- SPAR SKIN PANEL FOUND CRACK AR STA 120.3 DETAILS REFER ATTACHED FIG. TRANSFER REF NON- ROUTINE L/P 9130284 AND ORIGINAT ED BY V897399 THIS ITEM WAS REPAIRED IAW SRM 55-10-01-2R-11 REPAIR 11 AND
- [SDR CALA2021092701689](https://openairdocs.org/sdr/CALA2021092701689.md): Panel · cracked · Sep 27, 2021 · N34282 · Boeing 7378 · Empennage Structure
  > SUPPORT TASK EA 5510-01843 OP1 LH HORIZONTAL STABILIZER LOWER IN- SPAR SKIN PANEL FOUND CRACK AT STA 157.1 DETAILS REFER ATTACHED FIG. TRANSSFER REF NON- ROUTINE L/P 9130285 AND ORIGINA TED BY V897399 THIS ITEM WAS REPAIRED IAW SRM 55-10-01-2R-11 REPAIR 11 AND
- [SDR CALA2021063000995](https://openairdocs.org/sdr/CALA2021063000995.md): Connector · damaged · Jun 29, 2021 · N34282 · Boeing 737824 · Ice/Rain Protection System Wiring
  > ENG 2 COWL ANTI ICE LIGHT CAME ON AFTER T/OFF AND WOULD NOT GO O UT AT IDLE FOUND LOOSE CONNECTION AT PIN ON CONNECTOR D638. INSTALLED NEW CONTACT AND PERFORMED OPERATIONAL CHECK REF AMM 30-11-41 AND WDM 31-52-56. TEST PASSED, OKAY FOR SERVICE.
- [SDR CALA2020032100675](https://openairdocs.org/sdr/CALA2020032100675.md): Battery Pack · discharged · Mar 19, 2020 · N34282 · Boeing 737824 · Emergency Lighting
  > EMERGENCY LIGHT INOP AT AREA LIGHT AT SEAT 30,32.OVERHEAD CENTER G4 GALLEY,L2 DOOR INTERIOR AND EXTERIOR LIGHT INOP. REPLED AFT GALLEY LEFT BATTERY PACK M1673 PER AMM 33-51-06-960-805 TEST GOOD PN ON AD-D717-01-100 SN ON 177833 SN OFF 144554
- [SDR CALA2019092701636](https://openairdocs.org/sdr/CALA2019092701636.md): Unknown · malfunctioned · Sep 24, 2019 · N34282 · Boeing 737824 · Autopilot System
  > AC SHIFTED TO L WING LOW CORRECTED W/ RUDDR TRIM. AC THEN HAD UN CMMNDED RUDDER SHIFT TO RT LOW PER CREW DEBRIEF CAPT NOTICE YOKE SLIGHTLY OFF TO THE LEFT OR AILERON CORRECTED IT BY RUDDER TRIM. AFTER 30 SECONDS AIRCRAFT RUDDER SHIFTED TO THE RIGHT. REPORTS SH
- [SDR CALA2019062401059](https://openairdocs.org/sdr/CALA2019062401059.md): Aoa · malfunctioned · Jun 24, 2019 · N34282 · Boeing 737824 · Stall Warning System
  > SPEED LIMIT FLAG CAME ON IN FLT, STICK SHAKER ACTIVATED 6-7 TIMES IN FLT. NO HORIZ FLT DIR. ALL ON L TEST FOUND LEFT AOA SENSOR FAULTY. REMOVED AND REPLACED LT AOA SENSOR IAW AMM 34-21-05. TEST PASSED. NO FAULTS NOTED. OKAY FOR SERVICE.
- [SDR CALA2018110902330](https://openairdocs.org/sdr/CALA2018110902330.md): Doubler · cracked · Nov 8, 2018 · N34282 · Boeing 737824 · Fuselage Main, Plate/Skin
  > EGPR DOUBLER CRACKED IN ZONE 1 INTERIM REPAIR PERFORMED TO EGPR DOUBLER IAW ECRA 5331-02294 DTA DIP ACCOMPLISH INSP REQUIREMENTS ON OR BEFORE THE AIRCRACT REACHES 75000 TOT FLT CYCS PLANNING TO CONTACT ENGINEERING AFTER 68000 TOT FLT CYCS BUT BEFORE 69000 TOT
- [SDR CALA2018110302247](https://openairdocs.org/sdr/CALA2018110302247.md): Pressure Panel · cracked · Oct 30, 2018 · N34282 · Boeing 737824 · Fuselage Main, Bulkhead
  > HFEC FOUND ONE CRACK INDICATION ON CENTER WING BOX REAR SPAR VERTICAL PRESSURE WEB AT LBL 40.00. VERTICAL PRESS WEB HAS BEEN REPAIRED IAW SRM 57-10-10 REP 3.
- [SDR CALA2018110302246](https://openairdocs.org/sdr/CALA2018110302246.md): Skin · cracked · Oct 30, 2018 · N34282 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HAND HORIZONTAL STAB LOWER SKIN AT STAB STA 184.70 SHOWS CRACK INDICATION, 10 INCHES FWD OF TE SPAR. REPAIR RT HORIZONTAL STAB LOWER SKIN AT STA 184.70 PER SRM 55-10-01 REPAIR 11.
- [SDR CALA2018110202240](https://openairdocs.org/sdr/CALA2018110202240.md): Bulkhead · cracked · Oct 30, 2018 · N34282 · Boeing 737824 · Fuselage Main, Bulkhead
  > HFEC FOUND ONE CRACK INDICATION ON CENTER WING BOX REAR SPAR VERTICAL PRESSURE WEB AT RBL 40.00. VERTICAL PRESS WEB HAS BEEN REPAIRED IAW SRM 57-10-10 REP 3.
- [SDR CALA2018110302245](https://openairdocs.org/sdr/CALA2018110302245.md): Skin · damaged · Oct 29, 2018 · N34282 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STAB LOWER SKIN AT STA 120.30 CUT OUT ACCESS HOLES FOR RIB REPAIR. REPAIR RT HORIZONTAL STAB LOWER SKIN AT STA 120.30 PER SRM 55-10-01 REPAIR 11.
- [SDR CALA2018110202235](https://openairdocs.org/sdr/CALA2018110202235.md): Skin · cracked · Oct 29, 2018 · N34282 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STAB LOWER SKIN AT STA 157.10 SHOWS CRACK INDICATION 9 INCHES FWD OF TE SPAR. REPAIR RT HORIZONTAL STAB LOWER SKIN AT STA 157.10 PER SRM 55-10 -01 REPAIR 11.
- [SDR CALA2018110202234](https://openairdocs.org/sdr/CALA2018110202234.md): Skin · cracked · Oct 29, 2018 · N34282 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > RT HORIZONTAL STAB LOWER SKIN AT STA 138.70 SHOWS CRACK INDICATION 9 INCHES AFT OF LE SPAR. REPAIR RT HORIZONTAL STAB LOWER SKIN AT STA 138.70 PER SRM 55-10 -01 REPAIR 11.
- [SDR CALA2017121804500](https://openairdocs.org/sdr/CALA2017121804500.md): Unknown · odor · Dec 18, 2017 · N34282 · Boeing 737824 · Air Distribution System
  > FA REPORTED A FAINT BURNED RUBBER ODOR IN AFT GALLEY. ODOR WENT AWAY AFTER LEFT RECIRCULATION FAN WAS OFF/ON. CLEANED AND PERFORMED VISUAL INSPECTION OF AFT GALLEY APPLIANCES AND OPS CHECKED LEFT AND RIGHT HAND RECIRCULATION FANS NO FAULTS FOUND IAW 21-25-
- [SDR CALA2017112504211](https://openairdocs.org/sdr/CALA2017112504211.md): Light · inoperative · Nov 25, 2017 · N34282 · Boeing 737824 · Emergency Lighting
  > AFT LEFT OVERWING EXT EMERGENCY EXIT LIGHT INOP. RE-LAMPED EMERGENCY EXIT LIGHT REF MM 33-51-01. OPS CK OK.
- [SDR CALA2017091503200](https://openairdocs.org/sdr/CALA2017091503200.md): Lens · cracked · Sep 15, 2017 · N34282 · Boeing 737824 · Emergency Lighting
  > EMERGENCY SIGN LENS AT THE L1 DOOR FELL OFF AND CRACKED. REPLACED THE SIGN LENS IAW AMM 25-00-00. NO DEFECTS NOTED. OPS CHECKED GOOD.
- [SDR CALA2017061901892](https://openairdocs.org/sdr/CALA2017061901892.md): Skin · cracked · Jun 19, 2017 · N34282 · Boeing 737824 · Horizontal Stabilizer, Plate/Skin
  > LEFT HORIZONTAL STAB LOWER SKIN HAS A CRACK AT HSS 157. REPAIRED THE SKIN IAW SRM 55-10-01, REPAIR 11.
- [SDR CALA2017040400832](https://openairdocs.org/sdr/CALA2017040400832.md): Light · inoperative · Apr 4, 2017 · N34282 · Boeing 737824 · Emergency Lighting
  > EMERGENCY EXIT SIGN DOES NOT TURN ON. 122 SIGN ABOVE 2R FELL NEEDS REINSTALL. REPLACED LIGHT AND LENS. OPS NORMAL. OK FOR SERVICE.
- [SDR CALA2017040400831](https://openairdocs.org/sdr/CALA2017040400831.md): Sign · loose · Apr 4, 2017 · N34282 · Boeing 737824 · Emergency Lighting
  > EMERGENCY EXIT SIGN DOES NOT TURN OFF. 4R AFT EXIT SIGN 4R COVER FELL OFF. REINSTALLED EMERGENCY EXIT 4R.
- [SDR CALA2017040400830](https://openairdocs.org/sdr/CALA2017040400830.md): Sign · unsecure · Apr 4, 2017 · N34282 · Boeing 737824 · Emergency Equipment
  > EMERGENCY EXIT SIGN FELL OFF FROM REAR GALLEY DOOR 2R. SECURED EXIT SIGN, OK FOR SERVICE.
- [SDR CALA2015092400797](https://openairdocs.org/sdr/CALA2015092400797.md): Trim Motor · malfunctioned · Sep 24, 2015 · N34282 · Boeing 737824 · Stabilizer Actuator
  > STAB OUT OF TRIM LIGHT ON, WITH AUTOPILOT ELEC STAB TRIM INOPERATIVE, AFTER 20 MIN OF FLIGHT. REPLACED STAB TRIM MOTOR IAW AMM 27-41-71. PERFORMED & VERIFY IAW AMM 22-11-00. OPERATIONS CHECKED NORMAL. ACFT REMAINS A FULL CAT CAPABILITY. ACFT OK TO CONTINU
- [SDR CALA2014110501425](https://openairdocs.org/sdr/CALA2014110501425.md): Light · inoperative · Nov 5, 2014 · N34282 · Boeing 737824 · Emergency Lighting
  > SUPPORT TASK EMER LIGHT ON OVERHEAD BIN BETWEEN ROWS 11 & 12 ABC IS INOPERATIVE. RELAMPED EMER LIGHT AT ROW 11 & 12 ABC BINS. OPERATIONS CHECKED GOOD IAW AMM 33-51-03.
- [SDR CALA2014091801254](https://openairdocs.org/sdr/CALA2014091801254.md): Unknown · smoke · Sep 17, 2014 · N34282 · Boeing 737824 · Air Distribution System
  > FLIGHT ATTENDANT REPORTED SMOKE & FUMES AFT GALLEY & BEING LIGHT HEADED. RETURN TO BASE, SMOOTH TOUCHDOWN, 5500 LBS OVER MAX GROSS LAND WEIGHT. INSPECTED BOTH PACKS, GALLEYS & RAN BOTH ENGS AT HIGH POWER. ACCOMPLISHED PNEUMATIC BURN OUT TASK 21-00-01-100-80
- [SDR CALA2013111300843](https://openairdocs.org/sdr/CALA2013111300843.md): Transition Panel · corroded · Nov 13, 2013 · N34282 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO LT TRANSITIONAL PANEL HAS CORROSION FROM BS 727+10 TO 790. R & R TRANSITION PANEL FROM BS 727 TO 847 IAW SRM 51-40-02 & SRM 53-00-53.
- [SDR CALA2013111300840](https://openairdocs.org/sdr/CALA2013111300840.md): Skin · worn · Nov 13, 2013 · N34282 · Boeing 737824 · Engine Cowling System
  > NR 2 ENG, OTBD FAN COWL, SKIN BELOW UPPER RUB STRIP ON THE AFT END IS WORN. CUT OUT DAMAGED SECTION OF FAN COWL, FABRICATED & INSTALLED REPAIR PARTS IAW ECRA 7110-01902.
- [SDR CALA2013110800830](https://openairdocs.org/sdr/CALA2013110800830.md): Transition Panel · corroded · Nov 6, 2013 · N34282 · Boeing 737824 · Fuselage Miscellaneous Structure
  > AFT CARGO RT TRANSITION PANEL HAS CORROSION FROM BS 752 - 767. REPAIRED IAW SRM 53-00-53 REPAIR 5.

Next page: https://openairdocs.org/aircraft/N34282/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 = 'N34282' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N34282/reports

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