# Service difficulty reports: N17105

A list on [N17105](https://openairdocs.org/aircraft/N17105.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 · 98 reports

- [SDR CALA2026102120480](https://openairdocs.org/sdr/CALA2026102120480.md): Oven · smoke · Oct 18, 2026 · N17105 · Boeing 757224 · Buffet/Galleys
  > OVEN 204 SMOKING DURING USE. DEACTIVATED VIA CIRCUIT BREAKER IN FWD GALLEY IAW AMM 05-51-58-910-801-C1, REV 140. DURING OPS OF THE OVEN & FOUND HEAVY CONTAMINATION WITH FOOD, FOOD REMOVED AND TESTED AGAIN, ODOR REMAINS, OVEN C/B TRIPPED. IAW AMM 25-34-00-4
- [SDR CALA2026081718702](https://openairdocs.org/sdr/CALA2026081718702.md): Acm · faulty · Aug 15, 2026 · N17105 · Boeing 757224 · Cabin Cooling System
  > BURNING ODOR IN COCKPIT LOCKED LT PACK TRIPPED, FLIGHT DECK WENT FULL HOT THEREFORE CAUSING A HEAT/HOT ODOR COMPLIED WITH FORM 46-6020 PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-58, SMELLED, IT WAS A HEATING ODOR DUE TO THE LT PACK TEMP RISING, TURNED OFF
- [SDR CALA2026060916955](https://openairdocs.org/sdr/CALA2026060916955.md): Light · broken · Jun 8, 2026 · N17105 · Boeing 757224 · Emergency Lighting
  > SEAT 30C EMERGENCY AISLE PATH LIGHT BROKEN. REMOVE AND REPLACE 30C AISLE PATH LIGHTING, OPS CHK GOOD.
- [SDR CALA2026042215605](https://openairdocs.org/sdr/CALA2026042215605.md): Lamp · inoperative · Apr 21, 2026 · N17105 · Boeing 757224 · Emergency Lighting
  > R4 EMERGENCY SLIDE LIGHT INOP REMOVED AND REPLACED R4 EMERGENCY SLIDE LAMP. IAW AMM 33-51-06-962-001-001. OPS CHECK GOOD.
- [SDR CALA2026042015492](https://openairdocs.org/sdr/CALA2026042015492.md): Light · inoperative · Apr 17, 2026 · N17105 · Boeing 757224 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - R4 EXTERIOR EMERGENCY LIGHT INOP, REPLACED R4 EMERGENCY SLIDE LIGHT PER AMM 33-51-06. OPS CHECK GOOD.
- [SDR CALA2026013013441](https://openairdocs.org/sdr/CALA2026013013441.md): Smoke Detector · faulted · Jan 28, 2026 · N17105 · Boeing 757224 · Smoke Detection
  > ON DESCENT GOT A LAV SMOKE EICAS AND HORN FROM MID LAV. NO VISIB LE SMOKE OR ODOR PRESENT WHILE REMOVING SMOKE DETECTOR IN MID LAV FOUND ONE SCREW STRIPPED. REQUEST SHEET METAL ASSISTANCE. REMOVED STRIPPED SCREW PER SRM 51-40-02. REMOVED AND REPLACED LAV S SM
- [SDR CALA2025110510925](https://openairdocs.org/sdr/CALA2025110510925.md): Fanwheel · seized · Nov 3, 2025 · N17105 · Boeing 757224 · Engine (Turbine/Turboprop)
  > ENG EGT 941 2 MIN AFTER NORMAL ENG START. LOCKED FOR POSITIVE FIX PER CREW COMMENT, #1 ENGINE STARTED NORMALLY, THEN 2 MINUTES AFTER ENGINE START EGT SPIKED. CREW IMMEDIATELY SHUTDOWN ENGINE. ON VISUAL EXAMINATION, EXHAUST HAS NO DEBRIS, THE FAN DISK IS S
- [SDR CALA2025092409219](https://openairdocs.org/sdr/CALA2025092409219.md): Doubler · not reported · Sep 23, 2025 · N17105 · Boeing 757224 · Standard Practices/Structures
  > REPAIR FOUND ON LEFT FUSELAGE APPROX LOCATION OF BS 1787.45 + 27.5 TO BS 1830 LOCATED OVER LT HORIZONTAL STAB ABOUT 10" DOWN FROM VERTICAL STAB.REQUIRES REPLACEMENT DUE TO NO DOCUMENTATION OR DIP INFO FOR REP INSPECTIONS. REMOVED AND REPLACED DOUBLER STA 1787.
- [SDR CALA2025091708996](https://openairdocs.org/sdr/CALA2025091708996.md): Web · damaged · Sep 15, 2025 · N17105 · Boeing 757224 · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE TOP OF PYLON HYDRAULIC LINE BRACKET WORE INTO BOW TIE STRAP ON TOP OF PYLON. REPAIRED UPPER PLYLON WEB REF ECRA 5450-03044.
- [SDR CALA2025090808582](https://openairdocs.org/sdr/CALA2025090808582.md): Handle · worn · Sep 5, 2025 · N17105 · Boeing 757224 · Passenger/Crew Doors
  > L1 ENTREY DOOR UNABLE TO OPEN DOOR BY THE EXTERIOR HANDLE REMOVED L1 DOOR HANDLE ASSY, REPLACED CAM BASKET AND WORN HANDLE PARTS REF AMM 52-11-13
- [SDR CALA2025070206154](https://openairdocs.org/sdr/CALA2025070206154.md): Bellows · torn · Jun 29, 2025 · N17105 · Boeing 757224 · Engine (Turbine/Turboprop)
  > L ENG OVHT EICAS. EXTINGUISHED AT 1.30 EPR. PILOTS VERBALLY REPORTED,AT CRUISE, EICAS MESSAGE ALERT.THOTTLE MOVED TO IDLE EICAS GOES AWAY. RETURNED WHEN THROTTLE WAS MOVED JUST ABOVE IDLE. FOUND RIP IN PRECOOLER BELLOWS, FOUND FIRE ELEMENT IN CONTACT WITH SU
- [SDR CALA2025060905365](https://openairdocs.org/sdr/CALA2025060905365.md): Light · inoperative · Jun 8, 2025 · N17105 · Boeing 757224 · Emergency Lighting
  > AISLE ILLUMINATION EMERGENCY LIGHTS FROM ROW 34 TO 41 WONT LIGHT UP DURING EMERGENCY LIGHT TEST SWAPPED AFT BATTERIES PACKS TO IDENTIFY FAULT. NO HELP. MAY REQUIRE A NEW POWER SUPPLY. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW MM 33-51-07-022-020 OP
- [SDR CALA2025053005136](https://openairdocs.org/sdr/CALA2025053005136.md): Lavatory · full · May 28, 2025 · N17105 · Boeing 757224 · Waste Disposal System
  > ALL LAVS FULL, NEEDS LAV SERVICE ALL LAVS SERVICED AND OPERATIONAL
- [SDR CALA2025051504697](https://openairdocs.org/sdr/CALA2025051504697.md): Transmission · faulted · May 14, 2025 · N17105 · Boeing 757224 · Trailing Edge Flap Actuator
  > TE FLAP ASYM DURING 15 TO 20 EXTN ON APP. SPD 180IAS. PER CREW VERBAL EICAS MSG CLEARED AND BOTH SIDES WERE AT FLAPS 20. T/S PER FIM 27-51 FAULT TREE 805. FSEU 1 HAS RT FLAP XMT AS EXISTING FAULT. LEG 0 FAULT HISTORY SHOWS RT FLAP DRIVE FAULT MSG 315, FDE:FLA
- [SDR CALA2025051504680](https://openairdocs.org/sdr/CALA2025051504680.md): Charger · inoperative · May 14, 2025 · N17105 · Boeing 757224 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - ROW 34 TO ROW 41 SEAT EMERGECY LIGHT INOP DURING TEST REPLACED BATTERY PACK AND POWER SUPPLY AT AFT LOCATION M736 PER AMM 33-51-07-902-001 AND 33-51-07-862-054.AFTER OPS TEST FOUND TO BE WORK
- [SDR CALA2025042404199](https://openairdocs.org/sdr/CALA2025042404199.md): Bottle · low pressure · Apr 22, 2025 · N17105 · Boeing 757224 · Emergency Equipment
  > 1L PRESS LOW IN RED INSPECTED L1 PRESSURE GAGE FOR THE INFLATION CYLINDER REF AMM TASK 25-66-01-206-041, STILL WITHIN LIMITS. OK TO CONTINUE.
- [SDR CALA2025041103680](https://openairdocs.org/sdr/CALA2025041103680.md): Door · malfunctioned · Apr 8, 2025 · N17105 · Boeing 757224 · Passenger/Crew Doors
  > DOOR 2L NEEDS SOME TLC. MX NEEDING TO SLAM IT SHUT TO GET ENTRY DOOR LITE 2 GO OUT EWR+PDX OPERATED DOOR SEVERAL CYCLES. NO DEFECTS NOTED. EICAS WARNING AND OVERHEAD DOOR WARNING LIGHT EXTINGUISHED WITH DOORS CLOSED.
- [SDR CALA2024082300485](https://openairdocs.org/sdr/CALA2024082300485.md): Hose · faulty · Aug 21, 2024 · N17105 · Boeing 757224 · Waste Disposal System
  > FWD LAV HAD CONTINUOUS BLUE JUICE LEAK IN FWD LEFT CORNER OF LAV. REMOVED TOILET SHROUD FROM LAV "A". TOILET FOUND TO BE NOT OVERSERVICED. TOILET FLUSHES NORMALLY WITH NO LEAKS NOTED AT LAV TANK AND FLUSH COMPONENTS ON TOP OF LAV TANK. HAD LAV DUMPED AND A
- [SDR CALA2024053101653](https://openairdocs.org/sdr/CALA2024053101653.md): Warning Message · illuminated · May 31, 2024 · N17105 · Boeing 757224 · Engine Thrust Reverser
  > ON CLIMBOUT RECEIVED YELLOW REV ICON ABOVE RIGHT ENGINE EPR GAUG E REQUEST MEL FOR RIGHT ENG THRUST REVERSER INOP. PLACED RIGHT ENG T/R ON MEL DDP CW. RIGHT ENGINE THRUST REVERSER DEACTIVATED I.A.W. MEL 7831F. MEL AND DDP REQUIREMENTS CONTAINED IN 7831F COMP
- [SDR CALA2024022800589](https://openairdocs.org/sdr/CALA2024022800589.md): Skin · corroded · Feb 26, 2024 · N17105 · Boeing 757224 · Fuselage Main, Plate/Skin
  > B757-06-3-0241, AFT CARGO COMPARTMENT LH INTERNAL STRUCTURE STA 1400 AND NEXT TO STGR 25LH WITH CORROSION SPOT. REMOVED DAMAGED PARTS IAW B757 SRM 51-40-02, PERFORMED SURFACE A, 51-21-14 AND 51-21-15. ND OPEN HOLES HFEC INSPECTION IAW B757 NTM PART 6 51-00-19
- [SDR CALA2024022600541](https://openairdocs.org/sdr/CALA2024022600541.md): Web · corroded · Feb 24, 2024 · N17105 · Boeing 757224 · Fuselage Miscellaneous Structure
  > EXFOLIATION CORROSION AT STA 1862 BELOW ELEVATOR AUTOPILOT SERVOS ON WEB SHELF. REMOVED AND REPLACED WEB PLATE P/N 148N9203-16 AT STA 1862 B/W R BL30 TO LBL30 IAW SRM 51-40-02 AND DWG 148N9203. REINSTALLED 4EA FITTINGS FROM STA 1862 IAW SRM 51-40-02. PERFORMED
- [SDR CALA2024022600540](https://openairdocs.org/sdr/CALA2024022600540.md): Shelf · corroded · Feb 24, 2024 · N17105 · Boeing 757224 · Fuselage Miscellaneous Structure
  > B757-06-3-0272: EXFOLIATION CORROSION AT STA 1862 THROUGH ELEVST OR CONTROL ACCESS DOOR ON WEB SHELF. REMOVED AND REPLACED CHORD AT RBL30 STA 1862 IAW SRM 51-40-02 BATCH #0004239868 P/N 148N2122-1 DWG 148N9203 REV D. PERFORMED RII INSPECTION
- [SDR CALA2023101803105](https://openairdocs.org/sdr/CALA2023101803105.md): Oil Filter · warning message · Oct 16, 2023 · N17105 · Boeing 757224 · Turbine Engine Oil System
  > R OIL FILTER ADVISORY DISPLAYED ON CLIMB OUT AT APPROX 800 AGL REF LOGPAGE # 5962383 R ENG OIL FILTER BYPASS MEL APPLIED AND DAILY MAINTENANCE HAS BEEN ACCOMPLISHED PER MEL 7935B. DAILY MAINTENANCE REQUIREMENTS MUST BE COMPLIED WITH AS CONTAINE D IN LOG PAGE
- [SDR CALA2023053101722](https://openairdocs.org/sdr/CALA2023053101722.md): Stringer · damaged · May 29, 2023 · N17105 · Boeing 757224 · Fuselage Main, Longeron/Stringer
  > REF L/P4612658. STR24L BETWEEN STA680-700 DAMAGED CUT AND REMOVED STR24L FROM STA640-710 REF SRM53-00-03-2R-1 VERIFIED CUTOUT OF S24L STRINGER. PER AVO10784 REV A. C/W RR GMM PERFORMED HFEC PER AVO10784 REV A STEP 12. NO CRACKS INDICATION VERIFIED.040" INSURA
- [SDR CALA2023053101721](https://openairdocs.org/sdr/CALA2023053101721.md): Skin · damaged · May 29, 2023 · N17105 · Boeing 757224 · Fuselage Structure (General)
  > LAV SERVICE VEHICLE MADE CONTACT WITH AIRCRAFT WHILE SERVICING LAVATORY. GROUND DAMAGE SUSTAINED. DAMAGE SUSTAINED AROUND AFT LAV SERVICE PANEL. CORRECTION, DAMAGE SUSTAINED AT FWD LAV SERVICE PANEL NOT AFT LAV SERVICE PANEL AS PREVIOUSLY REPORTED. THE DAMAGE
- [SDR CALA2023022700565](https://openairdocs.org/sdr/CALA2023022700565.md): Flap System · none · Feb 27, 2023 · N17105 · Boeing 757200 · Flight Control System
  > TE FLAP DISAGEE LANDED FLAPS 20 FOUND ALT. FLAPS SET AT 20 AND TE & LE SWITCHES PUSH IN, RESET IT TO NORMAL, AND PERFORMED TASK 27-51-00-715-001 OPS CHECK GOOD
- [SDR CALA2022071801784](https://openairdocs.org/sdr/CALA2022071801784.md): Flap · gouged · Jul 16, 2022 · N17105 · Boeing 757224 · Trailing Edge Flaps
  > B757-06-3-0319: LEFT WING OUTBOARD MAIN FLAP, OUTBOARD LEADING EDGE GOUGED. TRANSCRIBED FROM HAECO GSO NRC# 9280692 REPAIRED LEFT WING O/B MAIN FLAP O/B L/E SKIN PER B757-200 SRM 5 7-53-01-2R-3. THE INSTALLED BLIND RIVETS REQUIRE INSPECTION EVER Y 2500 FLIGH
- [SDR CALA2022071301721](https://openairdocs.org/sdr/CALA2022071301721.md): Frame · cracked · Jul 13, 2022 · N17105 · Boeing 757224 · Fuselage Main, Frame
  > B757-53-3-0577 FRAME 1580RH - PSU SUPPORT RAIL ATTACHMENT CLIP T O FRAME INTERFACE - INBD RIVET, FRAME AFT SIDE HOLE CRACKED EXTE NDING FROM RIVET HOLE. TRANSCRIBED FROM HAECO GSO NR 9281088 THE ADDITIONAL 3 EA HOLES IAW B757-200 SRM 53-00-07-1A-3 AT STA HAECO
- [SDR CALA2022071301720](https://openairdocs.org/sdr/CALA2022071301720.md): Frame · cracked · Jul 13, 2022 · N17105 · Boeing 757200 · Fuselage Main, Frame
  > B757-53-3-0571 FRAME 1540LH - PSU SUPPORT TRAIL ATTACHMENT CLIP TO FRAME INTERFACE - INBD RIVET - FRAME AFT SIDE HOLE CRACKED EXTENDING FROM RIVET HOLE. TRANSCRIBED FROM HAECO GSO NR 9281089 REPAIRED CRACKED FRAME AT STA 1540 BETWEEN STR BL - 9L IAW B757- 200
- [SDR CALA2022071301716](https://openairdocs.org/sdr/CALA2022071301716.md): Flap · worn · Jul 11, 2022 · N17105 · Boeing 757200 · Wing Miscellaneous Structure
  > B757-06-3-0324 RIGHT WING IB MAIN FLAP LE AREA WORN NUMEROUS SPO TS, TRANSCRIBED FROM HAECO GSO NR 9280660
- [SDR CALA2022071301715](https://openairdocs.org/sdr/CALA2022071301715.md): Flap · gouged · Jul 11, 2022 · N17105 · Boeing 757200 · Trailing Edge Flaps
  > B757-06-3-0322 LEFT WING, INBOARD MAIN FLAP, LEADING EDGE GOUGED. TRANSCRIBED FROM HAECO GSO NR 9280709
- [SDR CALA2022070801683](https://openairdocs.org/sdr/CALA2022070801683.md): Bracket · cracked · Jul 7, 2022 · N17105 · Boeing 757224 · Fuselage Main, Frame
  > B757-53-3-0577 FRAME 1580RH - PSU SUPPORT RAIL ATTACHMENT CLIP T O FRAME INTERFACE - INBD RIVET, FRAME AFT SIDE HOLE CRACKED EXTENDING FROM RIVET HOLE. TRANSCRIBED FROM HAECO GSO NR 9281088
- [SDR CALA2022070801679](https://openairdocs.org/sdr/CALA2022070801679.md): Frame · cracked · Jul 7, 2022 · N17105 · Boeing 757224 · Fuselage Main, Frame
  > B757-53-3-0571 FRAME 1540LH - PSU SUPPORT TRAIL ATTACHMENT CLIP TO FRAME INTERFACE - INBD RIVET - FRAME AFT SIDE HOLE CRACKED EXTENDING FROM RIVET HOLE. TRANSCRIBED FROM HAECO GSO NR 9281089 REPAIRED CRACKED FRAME AT STA 1540 BETWEEN STR BL - 9L IAW B757- 200
- [SDR CALA2022062901604](https://openairdocs.org/sdr/CALA2022062901604.md): Seat Track · corroded · Jun 28, 2022 · N17105 · Boeing 757224 · Fuselage, Seat/Cargo Attach Fittings
  > SUPPORT TASK SEAT TRACK SUPPORT (P/N 141N5131-4) LOCATED BETWEEN STA 365-418 RBL 45 HAS CORROSION ON UPPER SURFACE TRANSCRIBED F ROM HAECO GSO NR 9280829
- [SDR CALA2022062701578](https://openairdocs.org/sdr/CALA2022062701578.md): Seat Track · corroded · Jun 25, 2022 · N17105 · Boeing 757200 · Fuselage, Seat/Cargo Attach Fittings
  > SUPPORT TASK SEAT TRACK SUPPORT PN 141N511-4 LOCATED BETWEEN STA 365-418 RBL 24 HAS CORROSION ON UPPER, TRANSCRIBED FROM HAECO G SO NR 9280828 NEW SUPPORT AND INTERCOSTAL IAW B757-200 SRM 51-40-02, BAC DW 14 1N5162 REV A AND 141N5130 REV E. HAECO GSO MECH V896
- [SDR CALA2022061701519](https://openairdocs.org/sdr/CALA2022061701519.md): Doubler · corroded · Jun 16, 2022 · N17105 · Boeing 757200 · Fuselage Main, Plate/Skin
  > EA-5100-02129-001 ANTENNA DOUBLER LOCATED AT STA 1500-1520 STR -2 8R IS CORRODED AND GOUGED ON INTERNAL SIDE, TRANSCRIBED FROM HAE CO GSO NR LP 9281209 AF343-2108-00 REV D. HAECO GSO MECH V898621 INSP QC467 REMOVED DAMAGED DOUBLER STA 1500-1520 S28R -S29R IAW
- [SDR CALA2022061301490](https://openairdocs.org/sdr/CALA2022061301490.md): Beam · corroded · Jun 12, 2022 · N17105 · Boeing 757224 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) CORROSION ON CREASE BEAM INNER CHORD AT LBL64 APP ROX STA 1630, TRANSCRIBED FROM HAECO GSO NRC 9280931
- [SDR CALA2022061301489](https://openairdocs.org/sdr/CALA2022061301489.md): Pressure Plate · corroded · Jun 12, 2022 · N17105 · Boeing 757224 · Fuselage Miscellaneous Structure
  > (SUPPORT TASK) LIGHT SURFACE CORROSION ON AFT DECK PRESSURE PLATE UPPER UPPER SURFACE LOCATED AT STA 1681 APPROX. RBL 60, TRANSCRIBED FROM HAECO GSO NR 9280939
- [SDR CALA2022022800517](https://openairdocs.org/sdr/CALA2022022800517.md): Generator · none · Feb 27, 2022 · N17105 · Boeing 757200 · Electrical Power System
  > CONTROL EICAS MESSAGE (L,R) GEN OFF DISPLAYED. (01=L,02=R) GEN O FF LGT ON AND (FAILED TO RESET, GEN RESET THEN RETRIPPED) 01 RESET L GEN AND IT TRIPPED AGAIN. PERFORMEDVISUAL INSPECTION OF LEFT IDG. LEFT IDG FEEDER CABLES BE PLACED ON MEL. LEFT IDG PLACED O
- [SDR CALA2021060700794](https://openairdocs.org/sdr/CALA2021060700794.md): Skin · scratched · Jun 5, 2021 · N17105 · Boeing 757224 · Fuselage Structure (General)
  > MOVE CREW FOUND SCRATCHES ON LEFT SIDE FORWARD OF DOOR 2L JUST AFT OF WING SCAN LIGHT LENS. AS REQUESTED BY ENGNR AND SM, PERFORMED NDT ULTRASONIC PER NTM PT 4-00-04-02, OLYMPUS 35 THICKNESS MEASUREMENT. PICTURES OF RESULTS ATTACHED BLENDED THE SKIN GOUGES IN
- [SDR CALA2019121602211](https://openairdocs.org/sdr/CALA2019121602211.md): Unknown · noise · Dec 13, 2019 · N17105 · Boeing 757224 · Standard Practices/Structures
  > CREW REPORTS LOUD NOISE UNDER FLOOR JUST AFT OF FLIGHT DECK DOOR. TRIED TURNING OFF RH AND LH RECIRC FANS NO HELP OPBLM HANN FLIGHT CREW REPORTED VERBALLY TO TECH SOUND COMING FWD OF FLT DECK DOOR. INSPECTED BOTH E&E COMPARTMENTS FOUND NO OBVIOUS DAMAGE WHEN R
- [SDR CALA2019092801641](https://openairdocs.org/sdr/CALA2019092801641.md): Shim · migrated · Sep 25, 2019 · N17105 · Boeing 757224 · Wing Miscellaneous Structure
  > SUPPORT TASK EA 5720-0341 REV A STEP 3 OF THIS EA SHIM MIGRATED 0.360, SHIM MIGRATION GREATER THEN 0.20 REQUIRES REPAIR THRU REF ST ENG N/R 0070121 ACCOMPLISHED ECRA 5720-03131 REV. A ON LH WING DRAG FITTING SHIM MIGRATION AND UPPER SKIN BLEND PART 1 INTERIM R
- [SDR CALA2019092301591](https://openairdocs.org/sdr/CALA2019092301591.md): Frame · corroded · Sep 9, 2019 · N17105 · Boeing 757224 · Fuselage Main, Frame
  > SUPPORT TASK EA5310-07027 (AD 2017-24-10) DURING PREPARATION (CL EANING) FOUND EXFOLIATION CORROSION ON FRAME OUTTER CHORD UNDER DOOR SWITHCH FITTING AT STA 1380 BETWEEN STR 23R AND STR 24R AS MARKED 034-036. REF ENG N/R 0069975 CHECKED LIMITS TO FRAME AT STA
- [SDR CALA2019091301527](https://openairdocs.org/sdr/CALA2019091301527.md): Girt Bar · worn · Sep 9, 2019 · N17105 · Boeing 757224 · Emergency Equipment
  > SUPPORT TASK EA 2560-02123 REV D L2 DOOR GIRT BAR FAILED MESUREMENT CHECK AT FWD POSITION. REF ST-SAA NR 0069614. REMOVED AND REPLACED L2 DOOR GIRT BAR IAW AMM 25-66-10-402-022 AREA FREE OF FOD.
- [SDR CALA2019091301526](https://openairdocs.org/sdr/CALA2019091301526.md): Girt Bar · worn · Sep 9, 2019 · N17105 · Boeing 757224 · Emergency Equipment
  > SUPPORT TASK EA 2560-02123 REV D L4 DOOR GIRT BAR FAILED MEASURE MENT CHECK AT FWD AND AFT POSITION. REF ST-ENG N/R 0069612 L4 DOOR GIRT BAR FAILED MEASUREMENT CHECK AT FORWARD AND AFT POSITION. REMOVED AND REPLACED L4 DOOR GIRT BAR IAW AMM 25-66-10-002-001 AN
- [SDR CALA2019083001445](https://openairdocs.org/sdr/CALA2019083001445.md): Structure · dented · Aug 25, 2019 · N17105 · Boeing 757224 · Cargo/Baggage Doors
  > (B757-06-3-0356) AFT CARGO DOOR FWD LWR CORNER HAS A DENT AS MAR KED 50-072. REF. ST. ENGINEERING N/R 0069791 REMOVED AND REPLACED AFT CARGO DOOR SEAL DEPCORNER PN NO. 654NO2 44-633 BATCH NO. 0003531247 PO NO SOS 1920075 IAW B757-200 SRM 5 1-40-02 AND B757-200
- [SDR CALA2019081651359](https://openairdocs.org/sdr/CALA2019081651359.md): Skin · damaged · Aug 1, 2019 · N17105 · Boeing 757224 · Fuselage Main, Plate/Skin
  > FOUND DAMAGE AT STA 418 STR 14R TO 15R. DENT MEASURE.040 DEPTH BY 1.2 BY.7 A/Y=17.5 PER SRM 53-0 0-01. REPAIRED IAW SRM 53-00- 01 REPAIR 29. THIS IS A CATAGORY B REPAIR.
- [SDR CALA2017102303747](https://openairdocs.org/sdr/CALA2017102303747.md): Altimeter · sticks · Oct 23, 2017 · N17105 · Boeing 757224 · Altimeter, Barometric/Encoder
  > STBY ALT STUCK AT 37500 FOR 500 FEET DURING DESCENT B4 IT BROKE FREE. REMOVED UNSERVICEABLE STBY ALT AND INSTALLED SERVICEABLE STBY ALTIMETER REF AMM 34-13-06-404-002, OPS CHECKED NORMAL.
- [SDR CALA2017091503192](https://openairdocs.org/sdr/CALA2017091503192.md): Wire Harness · faulty · Sep 15, 2017 · N17105 · Boeing 757224 · Light System Wiring
  > EXTERIOR EMERGENCY LIGHTING SYSTEM HAS ONE INOPERATIVE LIGHT LOCATED ON AFT CARGO DOOR. REPLACED WIRE HARNESS D41168P IAW WDM 33-27-21. OPS CHECKED NORMAL
- [SDR CALA2017090203030](https://openairdocs.org/sdr/CALA2017090203030.md): Cover · detached · Sep 2, 2017 · N17105 · Boeing 757224 · Emergency Lighting
  > L1 DOOR EXIT SIGN COVER DETACHED. INSTALLED THE COVER.

Next page: https://openairdocs.org/aircraft/N17105/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 = 'N17105' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N17105/reports

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