# Service difficulty reports: N19117

A list on [N19117](https://openairdocs.org/aircraft/N19117.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 · 102 reports

- [SDR CALA2026093020009](https://openairdocs.org/sdr/CALA2026093020009.md): Drag Fitting · not reported · Aug 30, 2026 · N19117 · Boeing 757224 · Nacelle/Pylon Structure
  > GENERATING DIP FOR LH ENGINE STRUT DIAGONAL BRACE ON WING FITTING REPEAT INSPECTIONS OF REPAIR PERFORMED ON ECRA 5720-03677
- [SDR CALA2026093020007](https://openairdocs.org/sdr/CALA2026093020007.md): Drag Fitting · unknown · Aug 30, 2026 · N19117 · Boeing 757224 · Nacelle/Pylon Structure
  > LH ENGINE STRUT DRAG FITTING TO WING SKIN HOLES. REPAIR PERFORMED ON ECRA 5720-03677. ACCOMPLISH INSPECTIONS IAW PART 2.3. OF EC5720-03677
- [SDR CALA2026092819869](https://openairdocs.org/sdr/CALA2026092819869.md): Skin · cracked · Aug 30, 2026 · N19117 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING INTER-SPAR LOWER SKIN, AROUND HOLE NR 27 UNDER PANEL 643BB REPAIR REPEAT INSPECTION REQUIREMENT PER ECRA 5720-03674AT RHS WING INTER-SPAR LOWER SKIN AROUND HOLE 27 INTERIM REPAIR AREA IAW PART 1 OF ECRA 5720-03674, COMPLETED.
- [SDR CALA2026091019363](https://openairdocs.org/sdr/CALA2026091019363.md): Skin · cracked · Aug 30, 2026 · N19117 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING INTER-SPAR LOWER SKIN AROUND HOLE NR 27 UNDER PANEL 643BB. ACCOMPLISH PERMANENT REPAIR PER PART 3 OF THE LATEST REVISION OF ECRA 5720-03674.
- [SDR CALA2026052516520](https://openairdocs.org/sdr/CALA2026052516520.md): Blowout Panel · missing · May 23, 2026 · N19117 · Boeing 757224 · Nacelle/Pylon, Main Frame
  > NR 2 ENG PYLON CIRCULAR ACCESS PANEL NOT INSTALLED. LEFT INBOARD SIDE OF NR 2 ENGINE PYLON MISSING BLOWOUT PANEL IPC 54-53-01-05 ITEM 245 MFG P/N 311N5049-9. INSTALLED NEW DOOR ASSY. ON NR 2 ENG. STRUT NACELLE PER AMM 54-53-01-404-005-001. ALSO INSPECTED AREA
- [SDR CALA2026031614580](https://openairdocs.org/sdr/CALA2026031614580.md): Unknown · odor · Mar 14, 2026 · N19117 · Boeing 757224 · Air Distribution System
  > ACRID SMELL NOTED IN FLT DECK AND CABIN WHEN ENGINE ANTI ICE O N IN ICING CONDITIONS. RAN NR 1 & 2 ENGINE SEPARATELY. OPS CHKD ENGINE ANTI ICE IAW AMM 30-21-00. 71-00-00. OPS CHK GOOD. NO FAULT FOUND. CAN NOT DUPLICATE ISSUE.
- [SDR CALA2026022314009](https://openairdocs.org/sdr/CALA2026022314009.md): Elec Connector · disconnected · Feb 21, 2026 · N19117 · Boeing 757224 · Light System Wiring
  > LAVATORY S EPL MONUMENT LIGHT INOPERATIVE. FOUND CONNECTOR DISCONNECTED UNDER SEAT 4B. RECONNECTED. MONUMENT LIGHT OPS CHECKED GOOD IAW AMM 33-51-11.
- [SDR CALA2025121712185](https://openairdocs.org/sdr/CALA2025121712185.md): Not Reported · not reported · Dec 15, 2025 · N19117 · Boeing 757224 · Standard Practices/Structures
  > LOW SPEED ABORT 60KTS. PERFORMED WALKAROUND AND INSPECTED BRAKES AND TIRES AND FOUND TO BE SATISFACTORY. BRAKE TEMPS WERE NORMAL. OK TO CONTINUE.
- [SDR CALA2025102010304](https://openairdocs.org/sdr/CALA2025102010304.md): Warning Light · malfunctioned · Oct 20, 2025 · N19117 · Boeing 757224 · Door Warning System
  > AFT CARGO DOOR LIGHT CAME ON DURING TAXI AFT CARGO DOOR INDICATION LIGH INOP..CARGO DOOR IS CLOSED, PUT IN MEL 5271E MEL 5271B APPROVED MEL 5271B, WE JUST COMPLIED WITH MEL, CARGO DOOR IS CLOSED AND CHECKED FROM OUT SIDE AND INSIDE. COMPLIED WITH MEL INTE
- [SDR CALA2025091108783](https://openairdocs.org/sdr/CALA2025091108783.md): Lamp · inoperative · Sep 10, 2025 · N19117 · Boeing 757224 · Emergency Lighting
  > EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - DOOR 1L EXTERIOR EMERGENCY LIGHT INOP REPLACED THE L1 DOOR EMERGENCY EXTERIOR SLIDE LIGHT REF AMM 33-51-06-962-001-001 OPS CK GOOD
- [SDR CALA2025090408452](https://openairdocs.org/sdr/CALA2025090408452.md): Bottle · no discrepancy · Sep 2, 2025 · N19117 · Boeing 757224 · Passenger/Crew Doors
  > PRESSURE GAUGE DOOR 2L IN RED CHECKING THE GAUGE FROM THE PROPER ANGLE, WITHIM LIMITS REF AMM 25-66-01-206-024
- [SDR CALA2025061905705](https://openairdocs.org/sdr/CALA2025061905705.md): Door · no discrepancy · Jun 16, 2025 · N19117 · Boeing 757224 · Passenger/Crew Doors
  > LEFT CENTER DOOR WILL NOT CLOSE COMPLIED WITH FIM 52-11 FAULT TREE 807. DOOR LATCHED NORMAL OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.
- [SDR CALA2025041503858](https://openairdocs.org/sdr/CALA2025041503858.md): Slide · unwanted deploy · Apr 12, 2025 · N19117 · Boeing 757224 · Escape Slide
  > THIS L/P CREATED FOR SDR REPORTING OF SLIDE DEPLOYMENT. SEE BAM NON-ROUTINE 002587892. FOR SLIDE REPLACEMENT AND OPERATION CHECK. LEFT O/W EXIT SLIDE DEPLOYED WHEN CB C5 ON P6-1 WAS CLOSED. MX FOUND THE AUTO FIRE SWITCH FOR THE LEFT FORWARD EXIT HATCH NOT ADJU
- [SDR CALA2025040303496](https://openairdocs.org/sdr/CALA2025040303496.md): Skin · damaged · Mar 31, 2025 · N19117 · Boeing 757224 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE AT STA 522, STR 4L. REPAIRED FUSELAGE SKIN REF SRM 53-00-01-2R-20, SEE NR 002538867 FOR WORK PERFORMED. ISSUE A DIP REF STEP 7 FOR INSPECTION REQUIR EMENTS. ZONE A AS FOLLOWS: INSPECTION THRESHOLD 375000 FLIGHT CY CLES AFTER AIRPLANE DELIVERY
- [SDR CALA2025031102690](https://openairdocs.org/sdr/CALA2025031102690.md): Light · inoperative · Mar 6, 2025 · N19117 · Boeing 757224 · Emergency Lighting
  > FWD AISLE EMERGENCY LIGHT AT SEAT 2AB INOP. REPLACED AISLE FLOOR PROXIMITY LIGHT IAW 33-51-11.
- [SDR CALA2024123001694](https://openairdocs.org/sdr/CALA2024123001694.md): Transmission · faulted · Dec 27, 2024 · N19117 · Boeing 757224 · Trailing Edge Flap Actuator
  > TE FLAPS DISAGREE EICAS COMPLIED WITH FLIGHT MAN PROCEDURE NORMA L LDG DURING INSPECTION, FOUND #5 FLAP TRANSMISSION OVERLOAD INDICATOR POPPED. SEE PIC. FOUND SCREW ASSY OF #5 FLAP TRANSMISSION CORRODED AND BURRS CAN BE FELT ON THREADS OF SCREW ASSY. FOUND BAL
- [SDR CALA2024122601661](https://openairdocs.org/sdr/CALA2024122601661.md): Transmission · tripped · Dec 24, 2024 · N19117 · Boeing 757224 · Trailing Edge Flap Actuator
  > TE FLAP DISAGREE BTWN F15 AND F20. SPEAKING WITH FLIGHT CREW THERE WERE NO FLIGHT ANOMOLIES QRH FOLLOWED FLAPS MOVED TO 20 WITH NO ISSUES. PERFORMED T/S PER FIM 27-51 FAULT TREE 808, FOUND FLAP TRANSMISSION #5(RH INBD) OVERLOAD INDICATOR TRIPPED. NO RECORDS O
- [SDR CALA2024121803115](https://openairdocs.org/sdr/CALA2024121803115.md): Hydraulic Line · leaking · Dec 17, 2024 · N19117 · Boeing 757224 · Hydraulic System, Main
  > WHILE INVESTIGATING LOW HYDRAULIC QTY, FOUND HYDRAULIC LEAK WHEN PRESSURIZED, ABOVE RT MAIN GEAR BLUE HYDRAULIC HOSES. DURING INSPECTION FOUND HOSE LEAKING ON RT MAIN LANDING GEAR, BLUE HYD HOSES REMOVED AND REPLACED TRUCK TILT HYD SYS FLEXIBLE PRESS LINE PER
- [SDR CALA2024041601109](https://openairdocs.org/sdr/CALA2024041601109.md): Nut · loose · Apr 13, 2024 · N19117 · Boeing 757224 · Engine (Turbine/Turboprop)
  > PARTIAL POWER LEFT ENGIN STARTED 15000 10 PERCEN THEN STOPPED 20 PERCNT LOWER CREW DEBRIEF - CREW STATED ENGINE MADE TARGET POWER ON TAKEOFF. AT 3K'' AT FIRST POWER REDUCTION ABOUT T MIN AFTER TO NOTICED LEFT ENGINE N1 20% LESS THAN RIGHT ENGINE BOTH EPR EVEN
- [SDR CALA2024040901013](https://openairdocs.org/sdr/CALA2024040901013.md): Flap System · warning message · Apr 5, 2024 · N19117 · Boeing 757224 · Trailing Edge Flap Control System
  > TE FLAP DISAGREE FLAP HANDLE AT 20 INDICATE FLAP 17 RAN QRC AND FLAPS DID PER FIM TASK 27-51 FAULT TREE 808 BLOCK 53 RESET OVERLOAD TRIP INDICATOR. AND MONITOR THE TE FLAP TRANSMISSION DURING FUTURE FLIGHTS. NO FURTHER ACTION REQUIRED.
- [SDR CALA2024040800998](https://openairdocs.org/sdr/CALA2024040800998.md): Pressure Valve · inoperative · Apr 4, 2024 · N19117 · Boeing 757224 · Pneumatic Distribution System
  > R BLEED OFF EICAS ON IN CRUISE. RESET OK. LOCKED DUE TO DIVERSION UNLOCKED AFTER REPLACEMENT OF PRSOV CREW REPORTS BLEED TRIPPED OFF AGAIN AND WOULD NOT RESET. WITH BLEED SWITCH IN OFF POSITION " BLEED OFF" AND "PACK OFF" LIGHTS ILLUMINATED YET RIGHT DUCT PRES
- [SDR CALA2024032200833](https://openairdocs.org/sdr/CALA2024032200833.md): Oven · fod · Mar 19, 2024 · N19117 · Boeing 757224 · Buffet/Galleys
  > AT FL360 60MIN FROM LAND ING-VERY STRONG ELECTRICAL BURN ODOR F C GALLEY. DISSAPATING SLOWLY NEED TO ACCOMPLISH SMOKE/ORDER IN FLIGHT DECK AND/OR CABINCONDITIONAL INSPECTION. IAW AMM 05-51-58-910-801-C1. FOUND COFFEEMAKER HEATING PLATE INOP & PAPER STICKER
- [SDR CALA2024030100617](https://openairdocs.org/sdr/CALA2024030100617.md): Light · disconnected · Mar 1, 2024 · N19117 · Boeing 757224 · Light System Wiring
  > FWD CABIN EMER FLOOD LT INOP FOUND FWD CABIN EMER FLOOD LT DISCONNECTED IN WALL. REINSTALLED FLOOD LT AND RELAMPED. OPS CK GOOD REF AMM 33-51-00 INSPECTED REPAIR AND VERIFIED OPERATION OF EMERGENCY LIGHTS PER AMM 33-51-00
- [SDR CALA2023091802812](https://openairdocs.org/sdr/CALA2023091802812.md): Sign · inoperative · Sep 15, 2023 · N19117 · Boeing 757200 · Emergency Lighting
  > F/A REPORTED VISIBLE SMOKE IN FWD CABIN. SMOKE WAS WHITE AND HAD ELECTRICAL SMELL. 19-3222-3-0001. SIGN OPS CHECK NORMAL FOR A FEW SECOUNDS THEN WENT LIGHTS BURNT OUT AGIAN. REMOVED LIGHT ORIGNAL BALLAST INSTALLED. ALL PARTS IN FLIGHT DECK. FUTHER T/S REQUIRED
- [SDR CALA2023090502711](https://openairdocs.org/sdr/CALA2023090502711.md): Hinge · corroded · Sep 4, 2023 · N19117 · Boeing 757224 · Fuselage, Door Hinge
  > THE LEVELING COMPOUND IS "HEAVED UP", AND THERE IS CORROSION UNDER IT, IN THE RECESS FOR THE CUTOUT IN THE UPPER DOOR HINGE, ON THE R2 DOOR.
- [SDR CALA2023090502710](https://openairdocs.org/sdr/CALA2023090502710.md): Door · corroded · Sep 4, 2023 · N19117 · Boeing 757224 · Service Doors
  > RI DOOR UPPER AND LOWER GATES ARE CORRODED ALONG THE EDGES.
- [SDR CALA2023082302622](https://openairdocs.org/sdr/CALA2023082302622.md): Pan · unknown · Aug 23, 2023 · N19117 · Boeing 757200 · Passenger/Crew Doors
  > REMOVE AND REPLACED L4 DOOR HANDLE PAN I/A/W SRM 51-40-02
- [SDR CALA2023062101959](https://openairdocs.org/sdr/CALA2023062101959.md): Control Unit · inoperative · Jun 19, 2023 · N19117 · Boeing 757224 · Flight Control System
  > A/C REQD 7 UNITS OF RT TRIM THRU FL340 AND 5 UNITS IN CRZ. L AIL LOOKS DEFLECTEDLEFT INBD AILERON PCA REQUIRES REPLACEMENT FOR PRECAUTIONARY REF. LOGPAGE 4909755. REMOVED LEFT INBD AILERON PCA PER AMM TASK 27-11-20-022-006 AND TASK PROGRESS SCREEN SHOTS ADDED
- [SDR CALA2022100602728](https://openairdocs.org/sdr/CALA2022100602728.md): Actuator · inoperative · Oct 6, 2022 · N19117 · Boeing 757224 · Rudder Tab Control System
  > UNABLE TO ADJUST RUDDER TRIM IN FLIGHT- AUTOPILOT ON OR OFF-NO D IFFERENCE GROUND TEST OF RUDDER TRIM SHOWS TRIM INTERMITTANTLY COMPLETELY INOP. FOLLOWED FIM 27-21 FAULT TREE 805, ELECTRICAL CHECKS AT TRIM ACT CANNON PLUG D1746 CHECK GOOD. FIM INDICATES TRIM
- [SDR CALA2022032100740](https://openairdocs.org/sdr/CALA2022032100740.md): Engine · power loss · Mar 21, 2022 · N19117 · Boeing 757200 · Fuel Control/Turbine Engines
  > RTO AT 70KT. LFT ENG DID NOT ACHIEVE TO THRUST. NOTICEABLE SPLIT ON THROTTLES. ACP FIM TASK 71-06 FAULT TREE 801 ( SLOW RESPONSE TO THRUST LEVER MOVEMENT). LOW IDLE SETTING AND HIGH IDLE CHECK TEST NO. 10 CHECKS OK. ACCELERATION AND DECELARATION TEST NO. 11
- [SDR CALA2022013100270](https://openairdocs.org/sdr/CALA2022013100270.md): Window · unlocked · Jan 31, 2022 · N19117 · Boeing 757200 · Flight Compartment Windows
  > INCREDIBLY LOUD SQUEAL FROM FO SIDE WINDOW STARTED AT FL240 AND COC KPIT COMMS DIFFICULT WILL REQUIRE POSITIVE FIX. SEAL AND WINDOW SHOW IN STOCK SFO ITEM UNLOCKED FOR UPDATE F/O INDICATED THAT NOISE CAME FROM THE SLIDING WINDOW, UPPER AFT CORNER, AND DID NOT
- [SDR CALA2021101101849](https://openairdocs.org/sdr/CALA2021101101849.md): Flap System · malfunctioned · Oct 11, 2021 · N19117 · Boeing 757224 · Trailing Edge Flap Control System
  > TE FLAP ASYM LANDED F15 ITEM LOCKED BY TOMC MGR DUE TO FLT CREW DECLARING AN EMERGENCY FOR LANDING CYCLE ALT FLAP AND SLAT SWITCH TO OPERATE FLAP HYDRAULICALLY. PERFORM TEST OF THE FSEU''S 1,2,3 AND NO FAULT FOUND. CREW INDICATED AT ONE POINT THE FLAP INDICATI
- [SDR CALA2020032100662](https://openairdocs.org/sdr/CALA2020032100662.md): Transmitter · faulty · Mar 16, 2020 · N19117 · Boeing 757224 · APU Oil System
  > AUXILIARY POWER UNIT EICAS MESSAGE APU OIL QTY DISPLAYED AND OIL QTY READS ADD (ON AIRPLANES WITH OIL QUANTITY TRANSMITTER) INDICATION ON STATUS PAGE ON CLIMBOUT THEN 0.25 OIL QUANTY SHOWS AT CRUISE REQUEST MEL 4994B. APU OIL VERIFIED FULL AT SIGHT GLASS APU V
- [SDR CALA2019102501815](https://openairdocs.org/sdr/CALA2019102501815.md): Oven · dirty · Oct 23, 2019 · N19117 · Boeing 757224 · Buffet/Galleys
  > OVEN 413 CONTINOUS SMOKE...DIVERTED TO LAS, PLEASE SEE LOG PAGE 3602103. LP 3602103- OVEN 3 EXTEREMLY DIRTY. FOUND OVEN DIRTY, PULLED BREAKERS ON OVEN 3. OK TO DEFER. PULLED AND COLLARED CIRCUIT BREAKER FOR G3. REMOVED AND REPLACED #3 AFT GALLEY OVEN IRW AMM
- [SDR CALA2018031900940](https://openairdocs.org/sdr/CALA2018031900940.md): Solenoid · failed · Mar 17, 2018 · N19117 · Boeing 757224 · Fixed Inner Doors
  > REJECTED TAKEOFF LOW SPEED FOR UNSECURE FLIGHT DECK DOOR. REMOVED AND REPLACED COCKPIT DOOR SOLEOID CATCH STRIKER ASSY IAW AMM 52-52-01-800-801C11. OPS CHECKED GOOD. DOOR OPEN LIGHT DOES NOT FLICKER WITH DOOR CLOSED.
- [SDR CALA2018010700089](https://openairdocs.org/sdr/CALA2018010700089.md): Battery Pack · discharged · Jan 7, 2018 · N19117 · Boeing 757224 · Emergency Lighting
  > EMERGENCY EXIT LOC SIGN ON MID FWD AND LEFT OVERWING EXIT LIGHT ASSY WAS REPORTED INOP. REPLACED POWER SUPPLY, BATTERY PACK AND EXIT LOC SIGN LIGHT ASSY REF AMM 33-51-07. OPS CHK NORMAL.
- [SDR CALA2017111704108](https://openairdocs.org/sdr/CALA2017111704108.md): Sensor · dirty · Nov 17, 2017 · N19117 · Boeing 757224 · Emergency Equipment
  > R4 DOOR WILL NOT DISARM. PERFORMED AMM 26-66-10-202-039, GIRT BAR AND FLOOR FITTING INSPECTION AND CHECK. INSPECTION REVEALED FOD IN THE FORWARD GIRT BAR SENSOR, CLEANED THE SENSOR. R4 DOOR ESCAPE SLIDE ARMED AND DISARMED NUMEROUS TIMES IAW AMM 25-65-00-002
- [SDR CALA2017111704107](https://openairdocs.org/sdr/CALA2017111704107.md): Sensor · faulty · Nov 17, 2017 · N19117 · Boeing 757224 · Emergency Equipment
  > R4 DOOR SLIDE LIGHT WILL NOT EXTINGUISH. FOUND S10224 SENSOR AT FAULT, REMOVED AND REPLACED IAW AMM 25-66-11. SYSTEM CHECKED OK.
- [SDR CALA2017091503176](https://openairdocs.org/sdr/CALA2017091503176.md): Unknown · odor · Sep 15, 2017 · N19117 · Boeing 757224 · Air Distribution System
  > FAINT SMOKE ODOR AFTER TAKEOFF. DISSIPATED QUICKLY. PERFORMED SMOKE & ODOR IN THE FLIGHT DECK INSPECTION IAW AMM 05-51-58-910-801C1. REMOVED AND REPLACED THE LEFT AND RIGHT CABIN AIR RECIRCULATION FILTERS IAW AMM 21-25-004-175,AND 21-25-02-404-175.
- [SDR CALA2017090803068](https://openairdocs.org/sdr/CALA2017090803068.md): Web · corroded · Sep 5, 2017 · N19117 · Boeing 757224 · Fuselage Miscellaneous Structure
  > BS 1390 WEB HAS CORROSION BELOW MAIN CABIN FLOOR PANEL ABOVE AFT CARGO DOOR CUT- OUT:REMOVED CORROSION ON WEB AT BS 1390 DOOR CUTOUT ORIG MAT THICK.071 MAT REMOVED.020 MAT REMAINING.051 FOUND TO BE OUT OF LIMITS IAW B757-200 SRM 53-60-15 FIG 101.CUT AND RE
- [SDR CALA2017090102971](https://openairdocs.org/sdr/CALA2017090102971.md): Frame · corroded · Sep 1, 2017 · N19117 · Boeing 757224 · Fuselage Main, Frame
  > AFT LAV SERVICE PAN CUT OUT AT FRAME 1680 RBL 8 HAS CORROSION.: REMOVED AND REPLACED LOWER FRAME AT BS 1680 IAW B757-200 SRM 51-40-02 PAR 4 AND 7 AND FIGS 8 AND 12. CORROSION OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL II IAW 19-5310-1-2688
- [SDR CALA2017090102980](https://openairdocs.org/sdr/CALA2017090102980.md): Pan · corroded · Aug 31, 2017 · N19117 · Boeing 757224 · Fuselage Miscellaneous Structure
  > LWR FUSELAGE AFT LAV SERVICE PAN HAS FRETTING CORROSION AROUND PAN LIP NO ALLOWABLE LIMITS FOUND IN SRM FOR LWR FUSELAGE AFT LAV SERVICE PAN. REMOVED AND REPLACED AFT LAV SERVICE PAN IAW B757-200 SRM 51-40-02 PAR 4,7 FIG 3,6,8,12.
- [SDR CALA2017082802918](https://openairdocs.org/sdr/CALA2017082802918.md): Shear Tie · corroded · Aug 28, 2017 · N19117 · Boeing 757224 · Fuselage Internal Mounting Structure
  > AFT LAV SERVICE PAN CUT OUT SHEAR TIE AT BS 1700 RBL 12 IS CORRODED. NO ALLOWABLE LIMITS FOUND FOR SHEAR TIE AT BS 1700 RBL 12, REMOVED, FABRICATED, LOCATED, DRILLED, & INSTALLED NEW SHEAR TIE IAW SRM 51-40-02 PAR 4 AND 7, FIG 8 AND 12.
- [SDR CALA2017082802917](https://openairdocs.org/sdr/CALA2017082802917.md): Shear Tie · corroded · Aug 28, 2017 · N19117 · Boeing 757224 · Fuselage Internal Mounting Structure
  > AFT LAV SERVICE PAN CUT OUT SHEAR TIE AT BS 1700 RBL 8 IS CORRODED. NO ALLOWABLE LIMITS FOUND FOR SHEAR TIE AT BS 1700 RBL 8, REMOVE D, FABRICATED, LOCATED, DRILLED, AND INSTALLED NEW SHEAR TIE IAW SRM 51-40-02 PAR 4 AND 7, FIG 8 AND 12.
- [SDR CALA2017082802916](https://openairdocs.org/sdr/CALA2017082802916.md): Frame · corroded · Aug 28, 2017 · N19117 · Boeing 757224 · Fuselage Main, Frame
  > AFT LAV SERVICE PAN CUTOUT FRAME AT STA 1700 RBL 8 HAS AREA OF CORROSION: REMOVED CORROSION ON FRAME AT BS 1700 RBL 8 ORIG MAT THICK IS.063" MAT REMOVED IS.022" MAT REMAINING IS.041" AND IS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-07 FIG 101 DETAIL II. REMOVED
- [SDR CALA2017082802915](https://openairdocs.org/sdr/CALA2017082802915.md): Stringer · corroded · Aug 28, 2017 · N19117 · Boeing 757224 · Fuselage Main, Longeron/Stringer
  > AFT LAV SERVICE PAN CUT OUT STRINGER 29R BS 1680-1700 IS CORRODED AND HAS DOUBLE DRILL HOLES: REMOVED AND REPLACED STR 29R BS 1620-1720 IAW SRM 51-40-02 PAR 4 AND 7. NO ALLOWABLE LIMITS FOR DOUBLE DRILLED HOLES AND REQUIRED REPLACEMENT IAW SRM 51-10-02 PAR 9
- [SDR CALA2017082802914](https://openairdocs.org/sdr/CALA2017082802914.md): Attach Bracket · corroded · Aug 28, 2017 · N19117 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFT LAV SERVICE PAN CUT OUT PAN UPPER ATTACH BRACKETS 2 EACH ARE CORRODED. NO ALLOWABLE LIMITS ON AFT LAV PAN UPPER ATTACH BRACKETS FOR CORROSION AND REQUIRED REPLACEMENT IAW SRM 51-10-02 PAR 9. REMOVED AND REPLACED UPPER ATTACH BRACKETS 2EA IAW SRM 51-40-02 P
- [SDR CALA2017082802913](https://openairdocs.org/sdr/CALA2017082802913.md): Doubler · corroded · Aug 28, 2017 · N19117 · Boeing 757224 · Fuselage Miscellaneous Structure
  > DOUBLER ON TOP OF AFT LAV SERVICE PAN IS DISBONDED AND CORRODED, NO ALLOWABLE LIMITS FOUND IN SRM FOR CORROSION ON DOUBLER. REMOVED AND REPLACED -9 DOUBLER PN146N3650-9 AT AFT LAV PAN IAW SRM 51-40-02 PAR 4 FIG 3,6,8.
- [SDR CALA2017082502846](https://openairdocs.org/sdr/CALA2017082502846.md): Frame · corroded · Aug 22, 2017 · N19117 · Boeing 757224 · Fuselage Main, Frame
  > GROUNDING STUDS AND HARDWARE HAS CORROSION AT BS 1480 STR 5R, UPON FURTHER EVALUATION FOUND CORROSION ON FRAME, REPAIRED TH EFRAME IAW SRM 53-00-07, REPAIR 1, FIG 201. GROUND STUDS AND HARDWARE REPLACED IAW SWPM 20-20-10, PG 25-40.
- [SDR CALA2017082102808](https://openairdocs.org/sdr/CALA2017082102808.md): Fuel Cell · corroded · Aug 21, 2017 · N19117 · Boeing 757224 · Fuel Storage
  > MAIN CABIN CENTER FUEL BOX UPPER SURFACE HAS CORROSION AT BS 980, LBL 60. BLENDED DAMAGED SECTION OF UPPER SKIN PANEL AND REPAIRED MAIN CABIN CENTER FUEL BOX UPPER SURFACE BS 980 LBL 60 IAW UNITED ECRA 5710-02614

Next page: https://openairdocs.org/aircraft/N19117/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 = 'N19117' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N19117/reports

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