# Service difficulty reports: N25705

A list on [N25705](https://openairdocs.org/aircraft/N25705.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 · 111 reports

- [SDR CALA2026101220272](https://openairdocs.org/sdr/CALA2026101220272.md): Lamp · inoperative · Oct 9, 2026 · N25705 · Boeing 737724 · Emergency Lighting
  > LH SIDE EMERGENCY LIGHT ON FUSELAGE INOPERATIVE. REPLACED LT SIDE FWD EMERGENCY LIGHT LAMP IAW AMM 33-51-04-960-801. OPS CHECKED GOOD
- [SDR CALA2026100620163](https://openairdocs.org/sdr/CALA2026100620163.md): Lens · loose · Oct 3, 2026 · N25705 · Boeing 737724 · Exterior Lighting
  > LEFT RETRACTABLE LDG LIGHT LENS SEEMS LOOSE REF AMM 33-42-02 REPLACED LH RETRACTABLE LDG LIGHT RETAINER ASSEMBLY DUE TO MISSING LENS, VERIFIED OPS OF LIGHT. PDA CREATED
- [SDR CALA2026100520103](https://openairdocs.org/sdr/CALA2026100520103.md): Lens · missing · Oct 3, 2026 · N25705 · Boeing 737724 · Exterior Lighting
  > LH RETRACTABLE LANDING LIGHT LENS FOUND MISSING. LEFT RETRACTABLE LDG LIGHT LENS SEEMS LOOSE REF AMM 33-42-02. REPLACED LH RETRACTABLE LDG LIGHT RETAINER ASSEMBLY DUE TO MISSING LENS, VERIFIED OPS OF LIGHT.
- [SDR CALA2026063017487](https://openairdocs.org/sdr/CALA2026063017487.md): Fitting · corroded · Jun 29, 2026 · N25705 · Boeing 737724 · Wing Main, Frame Structure
  > RIGHT WING AT RIB 27. THE LOWER FWD TENSION FITTING AT THE AFT ATTACH HOLE HAS PITTING CORROSION AT 11:00 O'CLOCK FACING INBD. REPAIRED R/W AT RIB 27 LOWER FWD TENSION FITTING AT AFT ATTACH HOLE IAW UAL AVO17710 REV ORIGINAL AND UAL ECRA 5720- 03661 REV ORIGIN
- [SDR CALA2026022714123](https://openairdocs.org/sdr/CALA2026022714123.md): Skin · cracked · Feb 23, 2026 · N25705 · Boeing 737724 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT RIGHT HORIZONTAL STAB LOWER SKIN AT HSS 129.50, INBD ROW, 9" FROM FRONT SPAR. CRACK LENGTH 1". REPAIRED RT HORIZONTAL STAB LOWER SKIN AT APPROX STA 129.5 IAW SRM 55-10-01-2R-11. ESFR ENTRY REQUIRED, DIP ENTRY REQUIRED. CATEGORY B REPAIR INS
- [SDR CALA2026022414028](https://openairdocs.org/sdr/CALA2026022414028.md): Spar · cracked · Feb 19, 2026 · N25705 · Boeing 737724 · Horizontal Stabilizer, Spar/Rib
  > FOUND CRACK ON RIGHT HORIZONTAL FRONT SPAR WEB AT APPROXIMATLY STA. 129.5 ON CIRCUMFERANCE OF LIGHTENING HOLE.REF BY AAR NR 100009960. REPAIRED RIGHT HORIZONTAL FRONT SPAR WEB AT APPROX STA 129.5 ON CIRCUMFERANCE OF LIGHTENING HOLE AS PER SRM 55-10-10-2R-1. WO
- [SDR CALA2026021813857](https://openairdocs.org/sdr/CALA2026021813857.md): Spar Web · corroded · Feb 16, 2026 · N25705 · Boeing 737724 · Wing Spar
  > LEFT WING FRONT SPAR BOOST PUMP SKIN CUTOUT UPPER SURFACE HAS CORRODED. REPAIRED LEFT WING FRONT SPAR WEB AT THE FUEL BOOST PUMP CUTOUT IAW ESR-WI 2024282-9-14664 WITH THE APROVAL OF EC/RA 5720-03617.
- [SDR CALA2025122412411](https://openairdocs.org/sdr/CALA2025122412411.md): Window Frame · cracked · Dec 22, 2025 · N25705 · Boeing 737724 · Fuselage Main, Structure
  > RIGHT NR 3 WINDOW FRAME FOUND CRACKED ON HOLES 3 & 4. PERFORMED REPAIR ON THE RT NR 3 WINDOW FRAME IAW EO 250450 REV. P1, P2, P3 AND IR, EA 5310-08195 REV. C, AND ECRA 5310-08750.
- [SDR CALA2025091508947](https://openairdocs.org/sdr/CALA2025091508947.md): Extinguisher · faulted · Sep 15, 2025 · N25705 · Boeing 737724 · Fire Protection System
  > WATER EXTINGUISHER AT 1L USED AS A PRECAUTION AND IT DID NOT OPERATE NORMALLY. CREW USED H2O EXTINGUISHER PRECAUTIONARILY ON CIGARETTE IN FWD LAV, NO SMOKE, NO ODOR, REMOVED AND REPLACED H2O EXTINGUISHER REF AMM 26-26-02
- [SDR CALA2025081207617](https://openairdocs.org/sdr/CALA2025081207617.md): Battery Pack · inoperative · Aug 11, 2025 · N25705 · Boeing 737724 · Emergency Lighting
  > AFT LEFT SECTION OF CABIN EMERGENCY LIGHT INOP. POWER SUPPLY BATTERY PACK REPLACED REF AMM 33-51-06-960-805, OPS CHECK GOOD.
- [SDR CALA2025062505853](https://openairdocs.org/sdr/CALA2025062505853.md): Cover · no discrepancy · Jun 21, 2025 · N25705 · Boeing 737724 · Escape Slide
  > 2L DOOR - FA STATES CAN FIT HAND BETWEEN DOOR AND SLIDE COVER. CHECKED AND FOUND 2L DOOR SLIDE COVER INSTALLED PER AMM 25-66-01-400-803. NO DEFECTS NOTED. CHECKED AND FOUND 2L DOOR SLIDE COVER INSTALLED PER AMM 25-66-01-400-803. NO DEFECTS NOTED.
- [SDR CALA2025052204908](https://openairdocs.org/sdr/CALA2025052204908.md): Trim System · malfunctioned · May 19, 2025 · N25705 · Boeing 737724 · Stabilizer Control System
  > STABILIZER FAILS TO TRIM NOSE UP ASSOCIATED SPEED TRIM FAIL LIGHT ILLUNINATED PER CREW, BOTH CAPT AND F/O SWITCHES WOULD NOT TRIM NOSE UP BUT TRIMMING DOWN WAS OK. INITIAL EVAL CYCLED STAB TRIM BREAKERS AND GOT BOTH ELECTRIC STAB TRIM SWITCHES TO MOVE UP AND D
- [SDR CALA2024121601531](https://openairdocs.org/sdr/CALA2024121601531.md): Battery · inoperative · Dec 14, 2024 · N25705 · Boeing 737724 · Fuel Selector/Shut-Off Valve
  > EMERGENCY FUEL SHUTOFF VALVE BATTERY NEEDS CHANGED DUE TO LIFE LIMIT REMOVED AND REPLACED EMERGENCY FUEL SHUT OFF VALVE BATTERY IAW AMM 28-22-14 OPS CHECK GOOD
- [SDR CALA2024121301492](https://openairdocs.org/sdr/CALA2024121301492.md): Transmitter · faulted · Dec 12, 2024 · N25705 · Boeing 737724 · Trailing Flap Position Indicating System
  > FLAPS STUCK AT 25 SETTING. REPLACED LH FLAP POS TRANSMITTER IAW AMM TASK 27-58-01-000-801 AND AMM TASK 27-58-01-400-801. ALL REQUIRED OP CHECKS TESTED OK.
- [SDR CALA2024112701322](https://openairdocs.org/sdr/CALA2024112701322.md): Stringer · corroded · Nov 2, 2024 · N25705 · Boeing 737724 · Fuselage Main, Longeron/Stringer
  > STRINGER 25L BETWEEN STA 827 & 847 IS CORRODED.CORROSION IS IN TWO EACH SPOTS. VERIFY REPLACEMENT STRINGER AS 146A3233-6, PO# 4429978. PER AVO 13590 REV B STEP 15. PERFORMED MATERIAL VERIFICATION, PO 4429978. TRIMMED OUT DAMAGED SECTION OF S-25L STRINGER FROM
- [SDR CALA2024112701323](https://openairdocs.org/sdr/CALA2024112701323.md): Skin · corroded · Oct 28, 2024 · N25705 · Boeing 737724 · Fuselage Main, Plate/Skin
  > FOUND CORROSION ON EXTERIOR SKIN AROUND LAV PAN OPENING AFTER OUTER LAV PAN REMOVAL.ADDED 3EA PICS. BLENDED OUT CORRODED LOWER SKIN REF SRM 51-10-02. THICKNESS OF SKIN REMOVED IS BEYOND ALLOWABLE LIMITS. ACCOMPLISHED STEPS 1. THROUGH 5. OF AVO 13590. REQUEST I
- [SDR CALA2024102900958](https://openairdocs.org/sdr/CALA2024102900958.md): Battery Pack · discharged · Oct 26, 2024 · N25705 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1675 FAILED CAPACITY CHECK.EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - REPLACED BATTERY PACK AS PER MM 33-51-06, OPS CKS GOOD
- [SDR CALA2024102900956](https://openairdocs.org/sdr/CALA2024102900956.md): Battery Pack · discharged · Oct 26, 2024 · N25705 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK M1672 FAILED CAPACITY CHECK.EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - REPLACED BATTERY PACK AS PER MM 33-51-06, OPS CKS GOOD
- [SDR CALA2024052101550](https://openairdocs.org/sdr/CALA2024052101550.md): Trim System · malfunctioned · May 16, 2024 · N25705 · Boeing 737724 · Auto Flight System
  > STAB OUT OF TRIM LIGHT ILLUMINATED ON TAKEOFF AT ABOUT 60 KTS REPLACED STAB OUT OF TRIM LIGHT M&E 29-3311-3-0062 REF FIM 22-11-851 AND AMM 22-11-00-740-806. ACCOMPLISHED DFCS AUTOTESTS PASSED.ACCOMPLISHED DFCS SPEED/STAB CHANNEL A & B TEST THAT ENGAGES AP A A
- [SDR CALA2023041401127](https://openairdocs.org/sdr/CALA2023041401127.md): Skin · unknown · Apr 12, 2023 · N25705 · Boeing 737 · Doors
  > EA5100-02345 REV E FOUND REINFORCINGT DOUBLER REPAIR ON AFT CARGO DOOR EXTERNAL SKIN AT 6OCLOCK FROM UPPER EDGE 13IN FROM AFT EDGE SIZE 13/12X9 REPAIR HAS A DEEP SCRATCH 3IN LONG REF AAR N/R 975221 REMOVED EXISTING DOUBLER AND REINSTALLED NEW DOUBLER ON AFT CA
- [SDR CALA2023041401126](https://openairdocs.org/sdr/CALA2023041401126.md): Unknown · dented · Apr 12, 2023 · N25705 · Boeing 737 · Fuselage Structure (General)
  > DENT AT FLIGHT DECK FLOOR AT WEB STA 260LBL 14 REF AAR N/R 974862 CUTOUT DAMAGED AREA AND INSTALLED REPAIR ON FLIGHT DECK FLOOR WEB BETWEEN STA 250 AND STA 270 AT LBL20 - RBL7.5 AS PER ECRA 5322-01118 THIS IS A CAT BREPAIR ON OR BEFORE THE ACCUMULATION OF 48,0
- [SDR CALA2023041401115](https://openairdocs.org/sdr/CALA2023041401115.md): Rib · cracked · Apr 12, 2023 · N25705 · Boeing 737 · Empennage Structure
  > R/H HORIZONTAL STAB FRONT SPAR INTERNAL RIB NO2 FWD UPPER FLANGE CRACKED (REF AAR N/R 975407) ACCOMPLISHED REPAIR AT R/H HS FRONT SPAR INTERNAL RIB NO2 FWD UPPER FLANGE AS PER ESR/RES WI 2020476-18-4125 AND ECRA 5510-03172. (WORK ACCOMPLISHED BY V930393)
- [SDR CALA2023041201098](https://openairdocs.org/sdr/CALA2023041201098.md): Unknown · cracked · Apr 12, 2023 · N25705 · Boeing 737 · Empennage Structure
  > R/H HORIZONTAL STAB FRONT SPAR INTERNAL RIB NO2 FWD UPPER FLANGE CRACKED (REF AAR N/R 975407) ACCOMPLISHED REPAIR AT R/H HS FRONT SPAR INTERNAL RIB NO2 FWD UPPER FLANGE AS PER ESR/RES WI 2020476-18-4125 AND ECRA 5510-03172. (WORK ACCOMPLISHED BY V930393)
- [SDR CALA2023041001090](https://openairdocs.org/sdr/CALA2023041001090.md): Unknown · dented · Apr 10, 2023 · N25705 · Boeing 737 · Fuselage Main, Structure
  > DENT AT FLIGHT DECK FLOOR AT WEB STA 260LBL 14 REF AAR N/R 974862 CUTOUT DAMAGED AREA AND INSTALLED REPAIR ON FLIGHT DECK FLOOR WEB BETWEEN STA 250 AND STA 270 AT LBL20 - RBL7.5 AS PER ECRA 5322-01118 THIS IS A CAT BREPAIR ON OR BEFORE THE ACCUMULATION OF 48,0
- [SDR CALA2023041001076](https://openairdocs.org/sdr/CALA2023041001076.md): Web · cracked · Apr 8, 2023 · N25705 · Boeing 737* · Fuselage Structure (General)
  > AFT WET AREA WEB STA 986.5 - STA 1016 AND RBL 33 - RBL 45 FOUND CRACKED. (REF AAR NR 975230) REMOVED AND REPLACED AFT WET AREA WEB AT STA 986.5 TO STA 1016 AND RBL 33- RBL 45 AS PER SRM 51-40-02-0G-0 AND DRAWING # 147A5700. ACCOMPLISHED BY V928494.
- [SDR CALA2023041001067](https://openairdocs.org/sdr/CALA2023041001067.md): Unknown · corroded · Apr 6, 2023 · N25705 · Boeing 737 · Fuselage Structure (General)
  > FWD PASSENGER COMP WET AREA R/H CORROSION ON INNER CHORD STA 277+14 TO 328+4 REF AAR N/R 974893 REMVOED AND REPLACED THE INNER CHORD STA 251 TO STA 360 AT FWD PASSENGER CABIN COMP WET AREA R/H PER B737 SRM 51-40-02-0G-0 AND DWG 141A8310 WORK ACCOMPLISHED BY V8
- [SDR CALA2023041001062](https://openairdocs.org/sdr/CALA2023041001062.md): Floorbeam · corroded · Apr 6, 2023 · N25705 · Boeing 737* · Fuselage Structure (General)
  > AFT WET AREA FLOOR BEAM STA 986,LBL 24 TO LBL 55 HAS SEVERAL SPOTS OF CORROSION.(REF AAR NR 975082) REMOVED CORROSION ON FLOOR BEAM STA 986.5 LBL TO ACCOMPLISHED FLOOR BEAM REPAIR AS PER SRM LBL 55 AS PER SRM 51-10-02-0G-0 ORIGINAL MAT. 53-70-51-2R-4. ALTERNAT
- [SDR CALA2023040601054](https://openairdocs.org/sdr/CALA2023040601054.md): Unknown · corroded · Apr 6, 2023 · N25705 · Boeing 737 · Standard Practices/Structures
  > FWD PASSENGER COMP WET AREA R/H CORROSION ON INNER CHORD STA 277+14 TO 328+4 REF AAR N/R 974893 REMVOED AND REPLACED THE INNER CHORD STA 251 TO STA 360 AT FWD PASSENGER CABIN COMP WET AREA R/H PER B737 SRM 51-40-02-0G-0 AND DWG 141A8310 WORK ACCOMPLISHED BY V8
- [SDR CALA2023040401034](https://openairdocs.org/sdr/CALA2023040401034.md): Web · cracked · Apr 4, 2023 · N25705 · Boeing 737 · Fuselage Structure (General)
  > AFT WET AREA WEB STA 986.5 - STA 1016 AND RBL 33 - RBL 45 FOUND CRACKED. (REF AAR NR 975230) REMOVED AND REPLACED AFT WET AREA WEB AT STA 986.5 TO STA 1016 AND RBL 33- RBL 45 AS PER SRM 51-40-02-0G-0 AND DRAWING # 147A5700. ACCOMPLISHED BY V928494.
- [SDR CALA2023040401033](https://openairdocs.org/sdr/CALA2023040401033.md): Unknown · corroded · Apr 4, 2023 · N25705 · Boeing 737 · Cabin Equipment/Furnishings
  > RH LOWER INNER CHORD FROM STA937 TO STA 992.5 HAS SPOTS OF CORROSION. (REF AAR NR 975073) REMOVED AND REPLACED R2 DOOR INNER CHORD P/N: 147A8540U8 PO#2004755, M&E 58-5300-3-0028 AND DRAWING #147A8501. ACCOMPLISHED BY V894534.
- [SDR CALA2023040401036](https://openairdocs.org/sdr/CALA2023040401036.md): Floorbeam · corroded · Apr 4, 2023 · N25705 · Boeing 737 · Fuselage Structure (General)
  > AFT WET AREA FLOOR BEAM STA 986.5,RBL24 TO RBL50 HAS SPOTS OF CORROSION. (REF AAR NR 975077) REMOVED CORROSION ON FLOOR BEAM STA 986.5 RBL 24 ACCOMPLISHED FLOOR BEAM REPAIR AS PER SRM TO RBL 50 AS PER SRM 51-10-02-0G-0. ORIGINAL MAT 53-70-51-2R-4 ALTERNATE 1
- [SDR CALA2023040401035](https://openairdocs.org/sdr/CALA2023040401035.md): Floorbeam · corroded · Apr 4, 2023 · N25705 · Boeing 737 · Fuselage Structure (General)
  > AFT WET AREA FLOOR BEAM STA 986,LBL 24 TO LBL 55 HAS SEVERAL SPOTS OF CORROSION.(REF AAR NR 975082) REMOVED CORROSION ON FLOOR BEAM STA 986.5 LBL TO ACCOMPLISHED FLOOR BEAM REPAIR AS PER SRM LBL 55 AS PER SRM 51-10-02-0G-0 ORIGINAL MAT. 53-70-51-2R-4. ALTERNAT
- [SDR CALA2023040401023](https://openairdocs.org/sdr/CALA2023040401023.md): Unknown · corroded · Apr 4, 2023 · N25705 · Boeing 737 · Fuselage Structure (General)
  > AFT WET AREA FLOOR BEAM STA 986.5,RBL24 TO RBL50 HAS SPOTS OF CORROSION. (REF AAR NR 975077) REMOVED CORROSION ON FLOOR BEAM STA 986.5 RBL 24 ACCOMPLISHED FLOOR BEAM REPAIR AS PER SRM TO RBL 50 AS PER SRM 51-10-02-0G-0. ORIGINAL MAT 53-70-51-2R-4 ALTERNATE 1
- [SDR CALA2023040401022](https://openairdocs.org/sdr/CALA2023040401022.md): Unknown · corroded · Apr 3, 2023 · N25705 · Boeing 737 · Fuselage Structure (General)
  > RH LOWER INNER CHORD FROM STA937 TO STA 992.5 HAS SPOTS OF CORROSION. (REF AAR NR 975073) REMOVED AND REPLACED R2 DOOR INNER CHORD P/N: 147A8540U8 PO#2004755, M&E 58-5300-3-0028 AND DRAWING #147A8501. ACCOMPLISHED BY V894534.
- [SDR CALA2023040401021](https://openairdocs.org/sdr/CALA2023040401021.md): Intercostal · corroded · Apr 3, 2023 · N25705 · Boeing 737 · Fuselage Structure (General)
  > AFT CARGO COMPARTMENT CORROSION @ WASTE TANK DUMP CHUTE ENCLOSURE SUPPORT STRUCTURE BETWEEN STA 847 AND 867, BETWEEN S-25L AND S-26L. (REF AAR N/R 975224) AFT CARGO COMP WASTE TANK DUMP CHUTE ENCLOSURE SUPPORT STRUCTURE BETWEEN STA 847 AND STA 867 FOUND OUT O
- [SDR CALA2023040301012](https://openairdocs.org/sdr/CALA2023040301012.md): Skin · cracked · Apr 3, 2023 · N25705 · Boeing 737 · Empennage Structure
  > R/H HORIZONTAL STAB LOWER SKIN HAS A 0.750 CRACK LOCAQTED AT ATAB STA 129.50 I/B RIVET ROW 19.00 FROM FRUNT SPAR REF NDTM UAL PART 6 SECTION 55-10-01 REF AAR N/R 974677 REMOVED EXISTING REPAIR BETWEEN STAB STA 138.7 AND 147.9 COTOUT DAMAGED AREA STA 129.5 19IN
- [SDR CALA2023040301011](https://openairdocs.org/sdr/CALA2023040301011.md): Waste Tank · corroded · Apr 3, 2023 · N25705 · Boeing 737 · Fuselage Structure (General)
  > AFT CARGO COMPARTMENT CORROSION @ WASTE TANK DUMP CHUTE ENCLOSURE SUPPORT STRUCTURE BETWEEN STA 847 AND 867, BETWEEN S-25L AND S-26L. (REF AAR N/R 975224) AFT CARGO COMP WASTE TANK DUMP CHUTE ENCLOSURE SUPPORT STRUCTURE BETWEEN STA 847 AND STA 867 FOUND OUT O
- [SDR CALA2023040300972](https://openairdocs.org/sdr/CALA2023040300972.md): Skin · cracked · Apr 1, 2023 · N25705 · Boeing 737 · Empennage Structure
  > R/H HORIZONTAL STAB LOWER SKIN HAS A 0.750 CRACK LOCAQTED AT ATAB STA 129.50 I/B RIVET ROW 19.00 FROM FRUNT SPAR REF NDTM UAL PART 6 SECTION 55-10-01 REF AAR N/R 974677 THRESHOLDS 56,000 TFC AND REPEAT INSP AT 9,000 F.C INTERVALS PER TABLE 204 WORK ACCOMPLISHE
- [SDR CALA2023040300971](https://openairdocs.org/sdr/CALA2023040300971.md): Structure · corroded · Apr 1, 2023 · N25705 · Boeing 737 · Fuselage Structure (General)
  > CABIN FLOOR STRUCTURE SHOWS EVIDENDE OF CORROSION AT L-2 DOOR INNER CHORD LOWER SURFACE AND AROUND ANCHOR NUTS STA 917 REF AAR N/R 975506 REMOVED AND REPLACED NEW CABIN FLOOR L-2 DOOR INNER CHORD FROM STA 897 TO STA 1016 LBL 60 PER REF B737 SRM 51-40-02-0G-0 A
- [SDR CALA2023033100937](https://openairdocs.org/sdr/CALA2023033100937.md): Beam · corroded · Mar 30, 2023 · N25705 · Boeing 737 · Fuselage Structure (General)
  > AFT WET AREA FLOOR BEAM STA 947.5 AND LBL 25 HAS EVIDENCE OF CORROSION REF AAR N/R 975299 ACCOMPLISHED FLOOR BEAM UPPER CHORD REPAIR AT STA 947.5 RBL 2 TO LBL 60 REF USED B737 SRM 53-70-51-2R-5 FIG 206 DETAIL A WORK ACCOMPLISHED BY V899763
- [SDR CALA2023032700898](https://openairdocs.org/sdr/CALA2023032700898.md): Floorbeam · corroded · Mar 27, 2023 · N25705 · Boeing 737* · Fuselage Structure (General)
  > AFT WET AREA FLOOR BEAM STA 947.5 AND LBL 25 HAS EVIDENCE OF CORROSION REF AAR N/R 975299 ACCOMPLISHED FLOOR BEAM UPPER CHORD REPAIR AT STA 947.5 RBL 2 TO LBL 60 REF USED B737 SRM 53-70-51-2R-5 FIG 206 DETAIL A WORK ACCOMPLISHED BY V899763
- [SDR CALA2023032400843](https://openairdocs.org/sdr/CALA2023032400843.md): None · corroded · Mar 22, 2023 · N25705 · Boeing 737 · Doors
  > FWD CARGO DOOR FWD CARGO DOOR AREA BELOW SCUFF PLATE WEB STA 440 TO STA 492.4 HAS SPOT EVIDENCE OF CORROSION REF AAR N/R 975096 REMOVED AND REPLACED FWD CARGO DOOR AREA BELOW SCUFF PLATES WEB STA 440 TO STA 492.4 PER REF B737 SRM 51-40-02-0G-0 AND SRM 51-40-05
- [SDR CALA2023032000814](https://openairdocs.org/sdr/CALA2023032000814.md): Door · corroded · Mar 20, 2023 · N25705 · Boeing 737* · Doors
  > FWD CARGO DOOR FWD CARGO DOOR AREA BELOW SCUFF PLATE WEB STA 440 TO STA 492.4 HAS SPOT EVIDENCE OF CORROSION REF AAR N/R 975096 REMOVED AND REPLACED FWD CARGO DOOR AREA BELOW SCUFF PLATES WEB STA 440 TO STA 492.4 PER REF B737 SRM 51-40-02-0G-0 AND SRM 51-40-05
- [SDR CALA2023031700778](https://openairdocs.org/sdr/CALA2023031700778.md): Unknown · corroded · Mar 16, 2023 · N25705 · Boeing 737* · Fuselage Structure (General)
  > FWD PASSENGER COMP WET AREA HAS EVIDENCE OF CORROSION ON INNER CHORD STA 380 AND LBL 64 REF AAR N/R 974900 CUTOUT DAMAGE AREA OF INNER CHORD STA 380 LBL64 AND INSTALLED SPLICE REPAIR REF AAR-MIA ESR 2020476-9 REV IR AND ECRA 5315-011878 WORK ACCCOMPLISHED BY V
- [SDR CALA2023031700773](https://openairdocs.org/sdr/CALA2023031700773.md): Frame · unknown · Mar 15, 2023 · N25705 · Boeing 737* · Fuselage Structure (General)
  > AS PER T/C EA 5310-04554 REV B OP004 ACCOMPLISHED THE R/H NO.1 WINDOW FRAME INSP AND PREVENTITIVE MOD AS PER T/C EA 5310-04554 REV B OP-004 ACCOMPLISHED THE R/H NO.1 WINDOW FRAME AND PREVENITIVE MODIFICATION WORK ACCOMPLISHED BY V917221
- [SDR CALA2023031500764](https://openairdocs.org/sdr/CALA2023031500764.md): None · corroded · Mar 15, 2023 · N25705 · Boeing 737* · Standard Practices/Structures
  > FWD PASSENGER COMP WET AREA HAS EVIDENCE OF CORROSION ON INNER CHORD STA 380 AND LBL 64 REF AAR N/R 974900 CUTOUT DAMAGE AREA OF INNER CHORD STA 380 LBL64 AND INSTALLED SPLICE REPAIR REF AAR-MIA ESR 2020476-9 REV IR AND ECRA 5315-011878 WORK ACCCOMPLISHED BY V
- [SDR CALA2023031500735](https://openairdocs.org/sdr/CALA2023031500735.md): Unknown · cracked · Mar 13, 2023 · N25705 · Boeing 737* · Fuselage Structure (General)
  > WING CENTER SECTION UPPER SURFACE HORIZONTAL PRESSURE WEB STA 665 RBL 40 CRACKED REF AAR N/R 974984 ACCOMPLISHED HORIZONTAL PRESSURE DECK WEB REPAIR BETWEEN STA 663 TO STA 675 FROM RBL38 TO EBL60 PER REF B737 SRM 53-40-51-2R-2 FIG 202 DETAIL A WORK ACCOMPLISHE
- [SDR CALA2023031300711](https://openairdocs.org/sdr/CALA2023031300711.md): Web · cracked · Mar 11, 2023 · N25705 · Boeing 737* · Wing Structure
  > INSTALL PERMANENT REPAIR AT RT W/W VERTICAL PRESSURE DECK WEB CRACKED BETWEEN RBL 40.0 AND RBL 45.61 REF LP 8609260 REF AAR N/R 974811 INTERVALS HFEC AND LFEC INSP PER B737 SRM 57-10-10-2R-3 STEP 7.B WORK ACCOMPLISHED BY V894534 ACCOMPLISHED VERTICAL PRESSURE
- [SDR CALA2023030900665](https://openairdocs.org/sdr/CALA2023030900665.md): Web · cracked · Mar 9, 2023 · N25705 · Boeing 737* · Wing Structure
  > INSTALL PERMANENT REPAIR AT RT W/W VERTICAL PRESSURE DECK WEB CRACKED BETWEEN RBL 40.0 AND RBL 45.61 REF LP 8609260 REF AAR N/R 974811 INTERVALS HFEC AND LFEC INSP PER B737 SRM 57-10-10-2R-3 STEP 7.B WORK ACCOMPLISHED BY V894534 ACCOMPLISHED VERTICAL PRESSURE
- [SDR CALA2023030900664](https://openairdocs.org/sdr/CALA2023030900664.md): Web · cracked · Mar 9, 2023 · N25705 · Boeing 737* · Fuselage Structure (General)
  > WING CENTER SECTION UPPER SURFACE HORIZONTAL PRESSURE WEB STA 665 RBL 40 CRACKED REF AAR N/R 974984 ACCOMPLISHED HORIZONTAL PRESSURE DECK WEB REPAIR BETWEEN STA 663 TO STA 675 FROM RBL38 TO EBL60 PER REF B737 SRM 53-40-51-2R-2 FIG 202 DETAIL A WORK ACCOMPLISHE

Next page: https://openairdocs.org/aircraft/N25705/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 = 'N25705' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N25705/reports

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