# Service difficulty reports: N29717

A list on [N29717](https://openairdocs.org/aircraft/N29717.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 · 70 reports

- [SDR CALA2026081018426](https://openairdocs.org/sdr/CALA2026081018426.md): Light · inoperative · Aug 8, 2026 · N29717 · Boeing 737724 · Emergency Lighting
  > FOUND RIGHT WING EXIT EMERGENCY LIGHT INOPERATIVE. R & R ALL FOUR RIGHT EMERGENCY EXIT ROW POWER SUPPLY FUSES IAW AMM 33-51-06-960-804. OPS CHKD GOOD. NO DISCREPANCIES NOTED.
- [SDR CALA2026042915814](https://openairdocs.org/sdr/CALA2026042915814.md): Fire Warning · false activation · Apr 28, 2026 · N29717 · Boeing 737724 · Fire Detection
  > LAV D FIRE ALARM ACTIVE LAV BOTTLE FIRE EXTINGUISHER DID NOT A CTIVATE PER FLIGHT CREW, NO SMOKE OR ODOR NOTICED WHEN ALARM WENT OFF. FA DID NOT TRY RESETTING SMOKE ALARM SOUND. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING
- [SDR CALA2026012613255](https://openairdocs.org/sdr/CALA2026012613255.md): Smoke Detector · no discrepancy · Jan 26, 2026 · N29717 · Boeing 737724 · Detection System
  > AFT LAVATORY ALARM WONT TURN OFF IAW FIM. 26-14 TASK 801. PERFORMED LAV SMOKE DET. SELF TEST. GREEN LED TESTED GOOD. NO SMOKE DETECTED, POSSIBLE DURING CATERING HOT FOOD SMOKE SEEPED IN. SMELLED CATERING FOOD BURNED DURING CATERING WITH AFT DOOR OPENED. RESE
- [SDR CALA2025123012512](https://openairdocs.org/sdr/CALA2025123012512.md): Unknown · odor · Dec 26, 2025 · N29717 · Boeing 737724 · Air Distribution System
  > SMELLED BURNING HYDRAULI C FLUID, 8000 FT THROUGH TD ON SNA ARRIVAL. PRESSURIZED HYD AND RAN PACKS FOR A WHILE, MOVED FLIGHT CONTROLS AND CHECKED FOR LEAKS ALSO CHECKED CABIN FOR SMELLS, UNABLE TO DUPLICATE THE SMELL, NO PREVIOUS HISTORY.
- [SDR CALA2025120811915](https://openairdocs.org/sdr/CALA2025120811915.md): Skin · delaminated · Dec 7, 2025 · N29717 · Boeing 737724 · Leading Edge Devices
  > LEFT WING, OTBD FLAP, AFT FLAP, INBD END, LOWER SKIN DEBONDED, L=8 X W=1INCHES. CLEANED, PREPPED, PERFORMED REPAIR AND RESTORED FINISHED ON LT WING AFT FLAP LOWER SKIN IAW SRM 57-53-01-2R-14, SRM 51-70-10-2R-0, SRM 57-53-01-1A-4, AMM 51-21-41-370-803, AND AMM
- [SDR CALA2025120811913](https://openairdocs.org/sdr/CALA2025120811913.md): Window Frame · damaged · Dec 7, 2025 · N29717 · Boeing 737724 · Fuselage Main, Structure
  > FOUND LIGHTNING STRIKE DAMAGE AT THE L3 WINDOW FRAME E-F POST BELOW THE LOWER NR 1 HOLE. PERFORMED THE REPAIR TO THE L3 WINDOW FRAME E-F POST REPAIRED IAW ECRA 5310-08733.
- [SDR CALA2025120811841](https://openairdocs.org/sdr/CALA2025120811841.md): Skin · delaminated · Dec 1, 2025 · N29717 · Boeing 737724 · Trailing Edge Flaps
  > RIGHT WING, OTBD FLAP, AFT FLAP, INBD END, LOWER SKIN DEBONDED, L=2 X W 1.5 INCHES. CLEANED, PREPPED, PERFORMED PERMANENT REPAIR, & RESTORED FINISH ON RT WING OTBD AFT FLAP LWR SKIN IAW SRM 57-53-01-2R-16, SRM 51-70-10-2R-0, AND AMM 51-21-99-300-801.
- [SDR CALA2025120811839](https://openairdocs.org/sdr/CALA2025120811839.md): Skin · delaminated · Dec 1, 2025 · N29717 · Boeing 737724 · Trailing Edge Flaps
  > RIGHT WING, OTBD FLAP, AFT FLAP, INBD END, UPPER SKIN WITH DISBONDED AREA, L=1 X W=1 INCHES. CLEANED, PREPPED, PERFORMED PERMANENT REPAIR AND RESTORED FINISH ON RT WING OTBD AFT FLAP UPPER SKIN IAW SRM 5 7-53-01-2R-16, SRM 51-70-10-2R-0, AND AMM 51-21-99-300-
- [SDR CALA2025060405250](https://openairdocs.org/sdr/CALA2025060405250.md): Bracket · damaged · Jun 2, 2025 · N29717 · Boeing 737724 · Emergency Equipment
  > GIRT BAR RIGHT SIDE SLIDE COVER BRACKET DOES NOT HOLD GIRT BAR UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID V941014 MAC RELATED WORK ORDER AND PRTR WALLACE, JACOB (V9410
- [SDR CALA2025032703246](https://openairdocs.org/sdr/CALA2025032703246.md): Structure · worn · Mar 24, 2025 · N29717 · Boeing 737724 · Fuselage Miscellaneous Structure
  > PACK BAY INSPECTION (RH) - AC BAY OUTBOARD CHORD HAS HOLE WORN THRU FROM LATCHCUT AND REMOVED THE DAMAGE PART OF THE LOWER CHORD, REQURED HFEC INSPECTION ALONG THE EDGE OF THE CUTOUT TO MAKE SURE NO CRACKS, REF SRM 57-10-13-2R-3 TASK 4E AND 4F. PERFORMED HFEC
- [SDR CALA2024112501276](https://openairdocs.org/sdr/CALA2024112501276.md): Proximity Sensor · faulty · Nov 25, 2024 · N29717 · Boeing 737724 · Leading Edge Slat Control System
  > ON APPROACH LE FLAP TRANSIT LIGHT ILLUMINATE..AND OVHD PANEL LE SLAT 5 ILLUM W/FLAPS 5 SELECT BITE TEST FSEU SHOWED MESSAGE 27-81208 SL5 PROX OUTBOARD PART INFO ADDED IN MATERIALS AND TOCS PART ODERED TO BE DELIVERED TO ZONE 4 SPLICED IN SL5 PROX OUTBOARD (S
- [SDR CALA2024093000717](https://openairdocs.org/sdr/CALA2024093000717.md): Bottle · empty · Sep 26, 2024 · N29717 · Boeing 737724 · Crew Oxygen System
  > O2 LEVEL DEPLETED TO 0 PSI. REMOVED AND REPLACED CREW OXYGEN CYLINDER REF AMM 12-15-21-600-801-001 LEAKS AND OPS CHECKS GOOD. FOUND OBSERVER MASK LEAKING FROM THE REGULATOR / STUCK IN THE TEST POSITION.
- [SDR CALA2024041001025](https://openairdocs.org/sdr/CALA2024041001025.md): Outflow Valve · failed · Apr 8, 2024 · N29717 · Boeing 737724 · Pressure Regulator/Outflow Valve
  > PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED UNABLE TO CONTROLL PERFORMED PRESSURIZATION SYSTEM GROUND TEST PER AMM TASK 21-31-00. BITE TEST SHOWED OUTFLOW VALV FAIL CODE. REMOVED AND REPLACED AFT OUTFLOW VALVE PER AMM 21-31-03. OP CHECK GOOD.
- [SDR CALA2023122003688](https://openairdocs.org/sdr/CALA2023122003688.md): Skin · dented · Dec 12, 2023 · N29717 · Boeing 737724 · Fuselage Main, Plate/Skin
  > FOUND 7" LONG B DENT @ LOWER FUS EXTDRNAL BELOW AFT CARGO BILGE BETWEEN S-26R AND S-27R STA 807 (REF AAR NR 9212566) INSTALLED DOUBLER AND FILLER REPAIR AT FUSELAGE SKIN BELOW AFT CARGO BILGE BETWEEN 526R AND S-27R STA 787+11.
- [SDR CALA2023112703482](https://openairdocs.org/sdr/CALA2023112703482.md): Floorbeam · corroded · Nov 26, 2023 · N29717 · Boeing 737724 · Fuselage Main, Floor Beam
  > AFT CABIN WET AREA FLOOR SUPPORT BEAM CORR. AT FASTNERS HOLES UPPER/LOWER SURFACES AT STA 986.5 LBL-22 TO LBL-44 MKD DOT 60-074 REF AAR N/R 9212715
- [SDR CALA2023112703478](https://openairdocs.org/sdr/CALA2023112703478.md): Skin · cracked · Nov 26, 2023 · N29717 · Boeing 737724 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND AT RT HORIZONTAL STAB. LOWER SKIN STAB STA 147.90 I/B FROM I/B FASTENER ROW 17 FWD FROM STAB REAR SPAR, CRACK LENGTH APPROX 0.500 REF AAR N/R 9212410
- [SDR CALA2023011300094](https://openairdocs.org/sdr/CALA2023011300094.md): Battery Pack · discharged · Jan 11, 2023 · N29717 · Boeing 737724 · Emergency Lighting
  > EMERGENCY LIGHTS CONTROLLED BY M1763 BATTERY INOP. REQUIRES BATTERY PACK D717-01-100. NIS IN CLE. REMOVED AND REPLACED M1763 BATTERY PACK REF MM 33-51-06. OPS CK OK. PARTS USED: 99-3351-3-0015,QTY:1
- [SDR CALA2023011300093](https://openairdocs.org/sdr/CALA2023011300093.md): Battery Pack · discharged · Jan 11, 2023 · N29717 · Boeing 737724 · Emergency Lighting
  > SEAT MOUNTED EMERGENCY EXIT LIGHTS FRIM ROW 29 AND AFT, AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN, AND R2 DOOR INTERIOR EMERGENCY EXIT SIGN INOP. FOUND M1762 BATTERY PACK P/N D717-01-100 NEEDS REPLACED. NIS IN CLE. REMOVED AND REPLACED M1762 BATTERY PACK REF MM
- [SDR CALA2022072501877](https://openairdocs.org/sdr/CALA2022072501877.md): None · faulty · Jul 25, 2022 · N29717 · Boeing 737 · Auto Flight System
  > A AUTOPILOT WOULD NEVER ENGAGE B A/P WOULD ENGAGE FOR A SECOND AND FAIL.SYSTEM SUSPECTS FAULTY ELEVATOR AUTOPILOT PRESSURE ENGAGE BUTTONS. REPLACED ELEVATOR A/P PRESSURE SWITCH, NO HELP. REPLACED ELEVATOR POSITION SENSOR M929 CAPABILITY.OPS CKS GOOD.
- [SDR CALA2020032100656](https://openairdocs.org/sdr/CALA2020032100656.md): Wire · cut · Mar 15, 2020 · N29717 · Boeing 737724 · Ice/Rain Protection System Wiring
  > VISUAL SPARKS FROM FWD CAPT AND FO WINDONS SMOKE AND ELECTRICAL SMELL FOLLOWED AND UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE FWD THE SMOKE /ODOR QUESTIONAIRE TO THE CAPT. AND FWD TO TOMC. INSPECT BOTH FWD FLIGHT DECK WINDOWS AND WHCU BITE. ADVISE TOM
- [SDR CALA2019041200560](https://openairdocs.org/sdr/CALA2019041200560.md): Slide · low pressure · Apr 9, 2019 · N29717 · Boeing 737724 · Escape Slide
  > DOOR 2R SLIDE PRESSURE GAUGE INDICATES NO PRESS URE. REMOVED AND REPLACED DOOR R2 SLIDE ASSY IAW AMM 25-66-01.DOOR OPENING AND CLOSING AS WELL AS ARMING AND DISARMING NORMAL.RII-
- [SDR CALA2017102303757](https://openairdocs.org/sdr/CALA2017102303757.md): Holder · loose · Oct 23, 2017 · N29717 · Boeing 737724 · Passenger/Crew Doors
  > AIRCRAFT AFT RIGHT GIRT BARREL HOLDER IS LOOSE. RETENSIONED BOTH SPRING STEEL GIRT BAR HOLDERS, GIRT BAR SECURED INTO CLIPS.
- [SDR CALA2017063002037](https://openairdocs.org/sdr/CALA2017063002037.md): Socket · faulty · Jun 30, 2017 · N29717 · Boeing 737724 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS PRTIALLY ILLUMINATED WITH SWITCH IN ARM POSITION. FOUND SOCKET L1065 RT SIDE THIRD FROM BACK BAD. REPLACED BOTH FUSES & SOCKETS RESET THE CIRCUIT BREAKER C1358 ON P-18. ALL EMERGENC Y LIGHTS OPS CHECKED NORMAL.
- [SDR CALA2017062301957](https://openairdocs.org/sdr/CALA2017062301957.md): Battery Pack · inoperative · Jun 23, 2017 · N29717 · Boeing 737724 · Emergency Lighting
  > DURING CHECK, FOUND THE R1 DOOR EMERGENCY EXIT SIGN ABOVE FLIGHT DECK DOOR INOPERATIVE. R & R THE BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR CALA2016110700866](https://openairdocs.org/sdr/CALA2016110700866.md): Warning System · false activation · Nov 7, 2016 · N29717 · Boeing 737724 · Trailing Flap Position Indicating System
  > REJECTED TAKEOFF AT 105KTS. FOR CONFIGURATION WARNING. FLAPS AT 5 DEGREES TRIM IN GREEN ARC. PERFORMED TAKE OFF FAULT ISOLATION AS PER FIM 27-81-00-810-811. FSEU AND PSEU BITE 27-51-00-810-801. NO DEFECTS NOTED AT THIS TIME. COULD NOT DUPLICATE. AC OK TO
- [SDR CALA2016050200283](https://openairdocs.org/sdr/CALA2016050200283.md): Engine · malfunctioned · May 2, 2016 · N29717 · Boeing 737724 · Engine (Turbine/Turboprop)
  > AT FL380 LT ENG LOST 50% POWER & SLIGHT VIBRATION OCCURRED, REDUCED TO IDLE. NO FURTHER VIBRATION OR ABNORMAL INDICATIONS, DECIDED TO OPERATE AT IDLE DECLARED EMER & DIVERTED. SUSPECT NR 4 BEARING FAILURE ON NR 1 ENG. R & R NR 1 ENG IAW WC 29-7100-1-0900, &
- [SDR CALA2015040800264](https://openairdocs.org/sdr/CALA2015040800264.md): Unknown · malfunctioned · Apr 8, 2015 · N29717 · Boeing 737724 · Fuel Controlling System
  > REJECTED TAKEOFF ON RNWY FOR NR 2 ENG AFTER STABILIZING 40% N1, ADVANCED THROTTLES & SELECTED TOGA. THROTTLES ADVANCED TOGETHER, BUT ENG 1 ACCEL NORMAL, WITH 2 HANGING UP AT 77.1% N1 AT ABOUT 50 KNOTS. ACCOMPLISHED FIM 73-26-00-810-803-F-00 NO FAULTS NOTED S
- [SDR 39NR20130829048A](https://openairdocs.org/sdr/39NR20130829048A.md): Bulkhead Web · cracked · Aug 29, 2013 · N29717 · Boeing 737724 · Fuselage Main, Bulkhead
  > DURING INSPECTION OF VERTICAL WEB AT BS 663, FOUND A CRACK 1.25 INCH LONG AT RBL 34, WL 196. REPAIRED IAW SRM 57-10-10. REPAIR NR 3 ALTERNATE NR 1.
- [SDR 39NR20130829049](https://openairdocs.org/sdr/39NR20130829049.md): Bulkhead Web · cracked · Aug 29, 2013 · N29717 · Boeing 737724 · Fuselage Main, Bulkhead
  > DURING INSPECTION OF VERTICAL PRESSURE WEB AT BS 663, FOUND TWO CRACKS,.5 INCH LONG AT LBL 35, WL 196 AND LBL 43, WL 197. REPAIRED PRESSURE WEB IAW SRM 57-10-10. REPAIR NR 3 ALTERNATE NR 2.
- [SDR 39NR20130829048](https://openairdocs.org/sdr/39NR20130829048.md): Bulkhead Web · cracked · Aug 29, 2013 · N29717 · Boeing 737219 · Fuselage Main, Bulkhead
  > DURING INSPECTION OF VERTICAL WEB AT BS 663, FOUND A CRACK 1.25 INCHES IN LENGTH AT RBL 34, WL 196. REPAIRED PRESSURE WEB IAW SRM 57-10-10, REPAIR NR 3, ALTERNATE NR 1.
- [SDR CALA2013011400040](https://openairdocs.org/sdr/CALA2013011400040.md): Floorbeam · corroded · Jan 14, 2013 · N29717 · Boeing 737724 · Fuselage Main, Floor Beam
  > FLOORBEAM, BS 967 HAS CORROSION AT FASTENERS HOLES BETWEEN LBL 12 TO LBL 18. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP REF ECRA 5311-01583.
- [SDR CALA2013011400039](https://openairdocs.org/sdr/CALA2013011400039.md): Frame · cracked · Jan 13, 2013 · N29717 · Boeing 737724 · Fuselage Main, Frame
  > RT FUSELAGE FRAME BS 380 BETWEENS STRINGERS 8 & 9R HAS CRACKED AT RIVETS ATTACHING BRACKET. INSTALLED REPAIR ANGLES DOUBLERS AND VERIFY ALL STEPS AND ATTACH HEAT TREAT FORM 43-0150 ARE COMPLIED REF ECRA 5311-01582.
- [SDR CALA2013011100036](https://openairdocs.org/sdr/CALA2013011100036.md): Angle · cracked · Jan 11, 2013 · N29717 · Boeing 737724 · Wing Miscellaneous Structure
  > RT WING HAS A CRACKED ANGLE SUPPORTING HYD LINE CLAMPS JUST OTBD OF NR 2 PYLON DIAGONAL STRUT AFT SIDE, REMOVED ANGLE, FABRICATED NEW ANGLE REF DWG 272A9125 AND REINSTALLED ANGLE, REF SRM 51-40-02.
- [SDR CALA2013011100025](https://openairdocs.org/sdr/CALA2013011100025.md): Angle · corroded · Jan 9, 2013 · N29717 · Boeing 737724 · Fuselage Main, Bulkhead
  > FORWARD CARGO BAY BULKHEAD BS 500D SUPPORT ANGLE HAS CORROSION JUST ABOVE S25R. INSTALLED SUPPORT ANGLE IAW SRM 51-40-02.
- [SDR CALA2013011100024](https://openairdocs.org/sdr/CALA2013011100024.md): Angle · corroded · Jan 9, 2013 · N29717 · Boeing 737724 · Fuselage Main, Bulkhead
  > FORWARD CARGO BAY BULKHEAD BS 500D SUPPORT ANGLE HAS CORROSION JUST ABOVE S25L. INSTALLED LT SUPPORT ANGLE IAW SRM 51-40-02.
- [SDR CALA2013011100020](https://openairdocs.org/sdr/CALA2013011100020.md): Transition Panel · corroded · Jan 8, 2013 · N29717 · Boeing 737724 · Fuselage Miscellaneous Structure
  > RT TRANSITION PANEL CORRODED BS 727 TO 767. R & R TRANSITION PANEL REF SRM 53-70-53 AND SRM 51-40-02.
- [SDR CALA2013011100019](https://openairdocs.org/sdr/CALA2013011100019.md): Cargo Track · cracked · Jan 8, 2013 · N29717 · Boeing 737724 · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO, RT CARGO TRACK CRACKED BS 727E, 747 AND 767 CORRODED BS 787 TO 847. INSTALLED NEW CARGO TRACK IAW SRM 51-40-02.
- [SDR CALA2013011100016](https://openairdocs.org/sdr/CALA2013011100016.md): Frame · cracked · Jan 8, 2013 · N29717 · Boeing 737724 · Fuselage Main, Frame
  > RT BS 296.4 LOWER STUB FRAME CRACKED LOWER END. COMPLIED WITH DOUBLER REPAIR IAW ECRA 5311-01581.
- [SDR CALA2013010700012](https://openairdocs.org/sdr/CALA2013010700012.md): Frame · cracked · Jan 4, 2013 · N29717 · Boeing 737724 · Fuselage Main, Frame
  > LEFT FUSELAGE FRAME BS 480 BETWEEN STRINGERS 8 AND 9L HAS CRACKED AT RIVET ATTACH BRACKET. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE A AND B IAW EA5310-04761, REV D.
- [SDR CALA2013010700011](https://openairdocs.org/sdr/CALA2013010700011.md): Frame · cracked · Jan 3, 2013 · N29717 · Boeing 737724 · Fuselage Main, Frame
  > RT FUSELAGE FRAME BS 480 BETWEEN STRINGERS 8 AND 9R HAS CRACKED AT RIVET ATTACH BRACKET. REPAIRED FRAME IAW EA 53-10-04716, REV D, OP 01.
- [SDR CALA2013010700010](https://openairdocs.org/sdr/CALA2013010700010.md): Angle · damaged · Jan 3, 2013 · N29717 · Boeing 737724 · Passenger/Crew Doors
  > L1 DOOR LT ANGLE DAMAGED BS 339. R & R L1 DOOR, LT ANGLE IAW SRM 51-40-02.
- [SDR CALA2013010700009](https://openairdocs.org/sdr/CALA2013010700009.md): Frame · cracked · Jan 3, 2013 · N29717 · Boeing 737724 · Fuselage Main, Frame
  > FRAME CRACKED BS 500C BETWEEN S8 AND 9R. MFEC INDICATIION AT INBD RIVET. REPAIRED CRACKED FRAME, REF EA 5310-04716, REV D, OP 1, FIG 3, STEPS 1, THROUGH 13.
- [SDR CALA2013010700008](https://openairdocs.org/sdr/CALA2013010700008.md): Frame · cracked · Jan 3, 2013 · N29717 · Boeing 737724 · Fuselage Main, Frame
  > RT FUSELAGE FRAME BS 440 BETWEEN STRINGERS 8 AND 9R HAS CRACK AT RIVET ATTACH BRACKET. REPAIRED CRACKED FRAME REF EA 5310-04716, REV D, OP 1, FIG 3, STEPS 1 THROUGH 13.
- [SDR CALA2013010700007](https://openairdocs.org/sdr/CALA2013010700007.md): Frame · cracked · Jan 3, 2013 · N29717 · Boeing 737724 · Fuselage Main, Frame
  > RT FUSELAGE FRAME, BS 827 BETWEEN STRINGERS 8 AND 9R HAS CRACKED AT RIVET ATTACHING BRACKET. REPAIRED RT FUSELAGE FRAME AT STA 827R BETWEEN STRINGERS 8 AND 9 REF, EA 5310-04716, REV D.
- [SDR CALA2013010400002](https://openairdocs.org/sdr/CALA2013010400002.md): Frame · cracked · Jan 2, 2013 · N29717 · Boeing 737724 · Fuselage Main, Frame
  > RT FUSELAGE FRAME, BS 500A BETWEEN STRINGERS 8 AND 9R HAS CRACK AT RIVET ATTACH BRACKET. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW EA5310-04716, REV D.
- [SDR CALA2013010400001](https://openairdocs.org/sdr/CALA2013010400001.md): Frame · cracked · Jan 2, 2013 · N29717 · Boeing 737724 · Fuselage Main, Frame
  > RT FUSELAGE FRAME BS 867 BETWEEN STRINGERS 8 AND 9R HAS CRACK AT RIVET ATTACH BRACKET. CUTOUT DAMAGED AREA AND FABRICATED, INSTALLED, TREATED, PRIMED REPAIR ANGLES, AND APPLIED CORROSION INHIBITING COMPOUND, ALL IAW EA 5310-04716, REV D, FIG 3.
- [SDR CALA2012123100904](https://openairdocs.org/sdr/CALA2012123100904.md): Floor Support · corroded · Dec 31, 2012 · N29717 · Boeing 737724 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT ANGLE BETWEEN RT OTBD G4 GALLEY MOUNTING BLOCKS (FWD AND AFT) BETWEEN STA 986.5 -1016 HAS CORROSION AT FWD END AREA. R & R FLOOR SUPPORT REF SRM 51-40-02.
- [SDR CALA2012123100905](https://openairdocs.org/sdr/CALA2012123100905.md): Floor Support · corroded · Dec 31, 2012 · N29717 · Boeing 737724 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BS 986.5 TO 1006 RBL 32 HAS CORROSION. R & R FLOOR SUPPORT IAW SRM 51-40-02.
- [SDR CALA2012123100903](https://openairdocs.org/sdr/CALA2012123100903.md): Floorbeam · corroded · Dec 30, 2012 · N29717 · Boeing 737724 · Fuselage Main, Floor Beam
  > FLOORBEAM, BS 986.5 HAS SURFACE CORROSION AT SEVERAL FASTENER HOLES ALONG THE AREA BETWEEN LBL 32 AND RBL 45. REPAIRED FLOORBEAM IAW ECRA 5321-014-98.
- [SDR CALA2012123100902](https://openairdocs.org/sdr/CALA2012123100902.md): Web · damaged · Dec 30, 2012 · N29717 · Boeing 737724 · Fuselage Miscellaneous Structure
  > WEB DAMAGED, BS 986.5 TO 1016 AT LBL 32 TO LBL 42. INSTALLED NEW WEB IAW DWG 147A5700 AND SRM 51-40-02.

Next page: https://openairdocs.org/aircraft/N29717/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 = 'N29717' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N29717/reports

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