# Service difficulty reports: N14106

A list on [N14106](https://openairdocs.org/aircraft/N14106.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 4 · 158 reports

- [SDR CALA2026101620413](https://openairdocs.org/sdr/CALA2026101620413.md): O-Ring · leaking · Oct 15, 2026 · N14106 · Boeing 757224 · Hydraulic System, Main
  > C-HYD QTY EICAS, LEAK COMING FROM DUAL PRESS/CASE DRAIN MODULE-C LOCATED IN HYD SERVICING BAY. LEAKING COMING FROM UPPER SWITCH BASE ASSY SEE PIC. PULLED AND COLLARED BOTH CENTER HYD PUMP CBS. REMOVED AND REPLACED O-RING ON UPPER PRESSURE SWITCH OF FILTER MOD
- [SDR CALA2026081418628](https://openairdocs.org/sdr/CALA2026081418628.md): Circuit Card · faulty · Aug 8, 2026 · N14106 · Boeing 757224 · Engine (Turbine/Turboprop)
  > RIGHT ENG OVHT EICAS, FL410 EGT SHOWED 587 AFTER ENG BLEED & PACK OFF. THRUST REDUCED. OVERHEAT LIGHT WENT OUT AT 1.39 EGT IAW FIM 26-11 FT 802. R & R AFOLTS CARD M10274, AMM 26-10-01/401.
- [SDR CALA2026051816338](https://openairdocs.org/sdr/CALA2026051816338.md): Warning Message · false activation · May 14, 2026 · N14106 · Boeing 757224 · Trailing Flap Position Indicating System
  > TE FLAP DISAGREE AFTER FLAP 25 SELECTION PERFORMED OPERATIONAL CHECK OF THE TE FLAPS. OPS CHECK GOOD. REF: AMM TASK 27-51-00-715-001. PERFORMED BITE TEST OF ALL THREE FSEUS. NO PRESENT FAULTS FOUND (SEE PICTURES). REF: FIM 27-51 FAULT TREE 805.
- [SDR CALA2026042815806](https://openairdocs.org/sdr/CALA2026042815806.md): Door Seal · worn · Apr 26, 2026 · N14106 · Boeing 757224 · Passenger/Crew Doors
  > LOUD SQUEAL OMMITTING FROM DOOR 1L TOP LEFT OF DOOR SEAL IMMEAD IATLY AFTER/T/O PERFORMED LEAK CHECK AND FOUND LEAK SOUND FROM BOTH UPPER CORNERS OF DOOR FRAME SEALS. UPON FURTHER INSPECTION FOUND DOOR FRAME WITH UNEVEN SURFACE FOR SEAL TO MATE WITH. APPLIED
- [SDR CALA2026030414305](https://openairdocs.org/sdr/CALA2026030414305.md): Plug · damaged · Mar 4, 2026 · N14106 · Boeing 757224 · Turbine Section
  > REMOVED PLUG HPNGVN IN REF TO L/P4936131 FOUND PLUG DAMAGE INSTALLED PLUG HPNGVN IN REF TO AMM 72-00-00-846-191-R02 VERIFIED INSTALLATION OF PLUG HPNGVN IN REF TO AMM 72-00-00-846-191-R02
- [SDR CALA2025120811827](https://openairdocs.org/sdr/CALA2025120811827.md): Slide · faulty · Dec 5, 2025 · N14106 · Boeing 757224 · Escape Slide
  > FOUND R1 DOOR SLIDE PRESSURE LOW. REMOVED R1 SLIDE. PARTIALLY INSTALLED NEW SLIDE, NEW SLIDE CAME WITH INCORRECT GIRT BAR. GIRT BAR NEEDS REPLACED IAW AMM TASK 25-66-01-404-044 UP TO AND INCLUDING STEP H(17). VERIFIED SLIDE INSTALLATION UP TO AND INCLUDIN
- [SDR CALA2025112111377](https://openairdocs.org/sdr/CALA2025112111377.md): Anti-Ice Valve · no discrepancy · Nov 19, 2025 · N14106 · Boeing 757224 · Air Intake Anti/De-Ice System
  > TIA VALVE LIGHT WITH EICAS WHEN THRUST IS BELOW 30 N1 ON TAXI NORMAL INDICATION PER CONDITIONS DESCRIBED. NO FURTHER ACTION NEEDED. IAW AMM 30-21-00.
- [SDR CALA2025100209521](https://openairdocs.org/sdr/CALA2025100209521.md): None · none · Oct 2, 2025 · N14106 · Boeing 757224 · Standard Practices/Structures
  > LIQUID OF UNKNOWN ORIGIN ALL ALONG RIGHT SIDE COCKPIT FLOOR. STRONG COFFEE SMELL ALSO. FLIGHT CREW SPILLED COFFEE DURING FLIGHT. SPILLAGE MOSTLY DRY UPON ARRIVAL. INSPECTED E+E NO FLUIDS FOUND.
- [SDR CALA2025091008728](https://openairdocs.org/sdr/CALA2025091008728.md): Wire · burned · Sep 8, 2025 · N14106 · Boeing 757224 · Electrical Power System Wiring
  > MAIN EQUIPMENT CENTER AT BS 395 RT UPPER POWER FEEDER IS BURNED. REMOVED AND REPLACED POWER FEEDER WIRE W3412-0003-210 AND W3412- 0010-210 IAW WDM 24-21-21 AND SWPM 20-10-21 21-30-13 AND 20-10-20 T97654 OPS CHECK OK IAW AMM 71-00-00-795-032 -R03.
- [SDR CALA2025091008724](https://openairdocs.org/sdr/CALA2025091008724.md): Wire Harness · burned · Sep 8, 2025 · N14106 · Boeing 757224 · Turbine Engine System Wiring
  > REF EA3611-01469. ENGINE 2 STRUT, UPPER SURFACE, RH SIDE, BY STA PPS 174.30, WIRE BUNDLE HAS CHAFING AND BURN MARKS. ESDR COMPLETED. REMOVED AND REPLACED POWER FEEDER WIRE W3412-0006-110 ON ENG #2 IAW AND M 24-21-21 AND SWPM 20-10-11 AMM 24-11-20-404-01 2 T011
- [SDR CALA2025090808587](https://openairdocs.org/sdr/CALA2025090808587.md): Bulkhead Web · gouged · Sep 6, 2025 · N14106 · Boeing 757224 · Fuselage Main, Bulkhead
  > AFTER RADOME HOLD SUPPORT BRACKET REMOVED, FOUND A GOUGE A T BULKHEAD FRONT FACE SKIN BS 200 LBL 15. ACCOMPLISHED REPAIR ON FWD BULKHEAD FRONT FACE SKIN WITH NO DEVI ARIOUS PER VT MAE EA 757-5310-13-A4089 REV- AND EC/RA #5310-0868 9. DIP BY PAGES CREATED PER
- [SDR CALA2025090508509](https://openairdocs.org/sdr/CALA2025090508509.md): Skin · cracked · Sep 3, 2025 · N14106 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING SKIN AND DRAG FITTING. HAD A CRACK INDICATION, NOTED AT HOLE NR 3 IN BOTH LAYERS. ACCOMPLISHED REPAIR PER ECRA 5720-03563 AND EA 757-572 -13-A4083 WITH NO DEVIATIONS.
- [SDR CALA2025090508507](https://openairdocs.org/sdr/CALA2025090508507.md): Skin · cracked · Sep 3, 2025 · N14106 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING SKIN AND DRAG FITTING. CRACK INDICATION NOTED AT HOLE NR 5 IN BOTH LAYERS. ACCOMPLISHED REPAIR PER ECRA 5720-03563 AND EA 757-572-13-A4083 WITH NO DEVIATIONS.
- [SDR CALA2025090508505](https://openairdocs.org/sdr/CALA2025090508505.md): Skin · cracked · Sep 3, 2025 · N14106 · Boeing 757224 · Wing, Plate/Skin
  > RIGHT WING SKIN & DRAG FITTING HAD A CRACK INDICATION NOTED AT HOLE NR 4 IN BOTH LAYERS. ACCOMPLISHED A REPAIR IAW ECRA 5720-03563 AND EA 757-572-13-A4083 WITH NO DEVIATIONS.
- [SDR CALA2025090508503](https://openairdocs.org/sdr/CALA2025090508503.md): Drag Fitting · cracked · Sep 3, 2025 · N14106 · Boeing 757224 · Wing, Attach Fittings
  > RIGHT WING SKIN AND DRAG FITTING. A CRACK INDICATION NOTED AT HOLE NR 2 IN BOTH LAYERS. ACCOMPLISHED A REPAIR IAW ECRA 5720-03563 AND EA 757-572-13-A4083 WITH NO DEVIATIONS.
- [SDR CALA2025082908259](https://openairdocs.org/sdr/CALA2025082908259.md): Skin · corroded · Aug 24, 2025 · N14106 · Boeing 757224 · Fuselage Main, Plate/Skin
  > TAIL AREA, APU INLET DOOR FWD SIDE, CUTOUT H AS EVIDENCE OF CORROSION. REPAIRED STRAP FOR THE AUXILIARY POWER UNIT AIR STA 1825.00 BETW EEN STG 3 TO STA 6 R/H IAW B757-200 53-80-15-2R-1.
- [SDR CALA2025082908258](https://openairdocs.org/sdr/CALA2025082908258.md): Bear Strap · cracked · Aug 24, 2025 · N14106 · Boeing 757224 · Fuselage Main, Plate/Skin
  > L1 DOOR SUROUND THE 7TH CRITICAL FASTENER HOLE. COUNTING RT TO LT IAW FIGURE -00 2 OF EA5330-04213 REV D, HAD A CRACK INDICATION AT THE BEAR STRAP L AYER. ACCOMPLISHED REPAIR IAW EA 757-5310-A4078 AND EA 5330-04213 REV D. OPERATION 2 & EC/RA # 5330-07569.
- [SDR CALA2025082808230](https://openairdocs.org/sdr/CALA2025082808230.md): Tee Fitting · corroded · Aug 23, 2025 · N14106 · Boeing 757224 · Fuselage Miscellaneous Structure
  > DURING BODY FAIRING REMOVAL FOUND EXFOLIATED T-CHORD AT BS 900, LOWER AREA. R & R TEE FITTING BS 900 BETWEEN LBL65 IAW SRM 51-40-02-0G-0, AND SRM 51-70-12-0G-0, STEP C, TABLE II.
- [SDR CALA2025082508090](https://openairdocs.org/sdr/CALA2025082508090.md): Stop Fitting · damaged · Aug 23, 2025 · N14106 · Boeing 757224 · Fuselage Main, Structure
  > (SDR) 53-5305-1-2060 - TAIL AREA, AFT POTABLE WATER SERVICE DOOR FWD CUTOUT DOORSTOP IS DAMAGED. DOT 23-059. REF: NR 130314. C/W SDR/SFR REPORTING ONLY REPAIRED AFT POTABLE WATER SERVICE DOOR FWD CUTOUT DOOR STOPS PE R EC/RA# 5361-01126 AND VT MAE EA 757-5360-
- [SDR CALA2025082508089](https://openairdocs.org/sdr/CALA2025082508089.md): Support Channel · corroded · Aug 23, 2025 · N14106 · Boeing 757224 · Fuselage Miscellaneous Structure
  > AFTER OPENING ACCESS PANEL 197LL, FOUND SUPPORT CHANNEL WTB L BL 6 WITH EXFOLLIATION, STA 1180 TO STA 1220. DOT 68-18. REF: NR 129950. C/W SDR/SFR REPORTING ONLY REMOVED AND REPLACED SUPPORT CHANNEL AT STA 1180 TO STA 1220 LBL 6 IAW B757-200 SRM 51-40-02-OG-0
- [SDR CALA2025082508072](https://openairdocs.org/sdr/CALA2025082508072.md): Skin · dented · Aug 13, 2025 · N14106 · Boeing 757224 · Fuselage Main, Plate/Skin
  > (SDR) LP#5082799 DENT ON LHS FUSELAGE STA 620-STA 640, S21L TO S 22L(REPAIR PER SRM) REF:NR130571 SFR REPORTING ONLY SDR REPORTING SFR #1610 HAS BEEN UPDATED. RII VERIFIED JOB PERFORMED.
- [SDR CALA2025060605330](https://openairdocs.org/sdr/CALA2025060605330.md): Pressure Switch · faulted · Jun 4, 2025 · N14106 · Boeing 757224 · Flight Control System
  > STAB TRIM LIGHT ON O/H PANEL AND EICAS ILLUM AFTER T/O. ACCOMPLI SHED NON NORMAL. REMOVED AND REPLACED RIGHT BRAKE PRESSURE SWITCH IN REF AMM 27-41-07. LEAK CHECK GOOD. PERFORMED THE STABILIZER TRIM MODULE TEST IN REF 27-09-00-712-037 UP TO AND INCLUDING (4)(
- [SDR CALA2025031302747](https://openairdocs.org/sdr/CALA2025031302747.md): Relief Valve · damaged · Mar 10, 2025 · N14106 · Boeing 757224 · Cabin Pressure Control System
  > FOUND LOWER CABIN POSITIVE PRESSURE RELIEF VALVE MISSING LOWER FLAPPER. UPPER FLAPPER WAS REMOVED AND DEFERED ON LOG 3881765. FLAPPER SHAPE IS HALF CIRCLE OF 3 INCHES RADIUS. LOWER CABIN PRESSURE RELIEF VALVE CDL ON LOG 3881765
- [SDR CALA2025010301775](https://openairdocs.org/sdr/CALA2025010301775.md): Cover · detached · Jan 1, 2025 · N14106 · Boeing 757224 · Emergency Lighting
  > EMERGENCY EXIT COVER SNAPPED OFF SEAT 27C RESECURRED EXIT ROW COVER AT SEAT 27C
- [SDR CALA2024110801078](https://openairdocs.org/sdr/CALA2024110801078.md): Elec Connector · dirty · Nov 6, 2024 · N14106 · Boeing 757224 · Engine Fuel System Wiring
  > CTRL SW ENG DID SHUT DOWN BUT STRONG FUEL SMELL IMMED AFTERWARD SEE LP 9791798 - FOLLOWING MULTIPLE ENGINE RUNS AND NORMAL SHUTD OWNS, NO SMELL OR ODOR WAS NOTICED FOLLOWING ENGINE 1 SHUTDOWNS. OK TO CONTINUE. SEE REFERENCED LP FOR PARENT WRITE UP. ON LEFT ENG
- [SDR CALA2024093000721](https://openairdocs.org/sdr/CALA2024093000721.md): Skin · damaged · Sep 25, 2024 · N14106 · Boeing 757224 · Leading Edge Devices
  > NR 6 LEADING EDGE SLAT DAMAGE, APPROXIMATELY 66 SQUARE INCH SECTION OF THE INBOARD TRAILING EDGE WEDGE DEPARTED THE AIRCRAFT.
- [SDR CALA2024010500043](https://openairdocs.org/sdr/CALA2024010500043.md): Plate · cracked · Jan 4, 2024 · N14106 · Boeing 757224 · Wing Main, Frame Structure
  > RT WING TE WIGGLE PLATE IS CRACKED, LOCATED JUST AFT OF RT WING JACK PAD. REF AMES NR 165960-0600-0001 REMOVED AND REPLACED RT WING TE WIGGLE PLATE IAW B757 SRM 51-40- 02 PARA 4. SEE BACK FOR PARTIAL WORK ACCOMPLISHED.
- [SDR CALA2023121103621](https://openairdocs.org/sdr/CALA2023121103621.md): Cowling · damaged · Dec 8, 2023 · N14106 · Boeing 757200 · Nacelle/Pylon, Main Frame
  > PDA 1 UPON ARRIVAL, PILOT FOUND OIL ACCESS SERVICING DOOR RIPPED OFF FROM #1 ENGINE, SEE ORIGINAL LOG PAGE 6497592. ALSO, COMPLETED AN ESFR (SDR # 1034535) REPORT CONSULTED TOMC AND ORD ENGINEERING. NO CDL RELIEF, HOWEVER, POSSIBLE RELIEF WITH TRM 7110-01125
- [SDR CALA2023030900669](https://openairdocs.org/sdr/CALA2023030900669.md): Bearing · none · Mar 9, 2023 · N14106 · Boeing 757* · Doors
  > DOOR 1R VERY DIFFICULT TO ARM GIRT BAR BINDING DURING ARM/DISARM. FOUND FORWARD ROD END BEARING ASSY SHEARED BETWEEN GIRT BAR MECHANISM AND DOOR LOWER TORQUE TUBE. REMOVED ROD END BEARING ASSY. REF IPC 52-11-20-20A ITEMS 290 & 295. INSTALLED NEW SERVICEABLE
- [SDR CALA2023022700560](https://openairdocs.org/sdr/CALA2023022700560.md): Cowling · missing · Feb 27, 2023 · N14106 · Boeing 757200 · Nacelle/Pylon Structure
  > PDA 2 MISSING MASTER CHIP DETECTOR ACCESS PANEL 424CR ON ENG 2. DIMENSIONS 5X7 INCHES. AIPC REF 71-11-04. REMOVED AND REPLACED ENGINE #2 FAN COWL RH OUTBOARD PER EC/RA #5420-01600. REF AMM 71-11-04.
- [SDR CALA2023010600047](https://openairdocs.org/sdr/CALA2023010600047.md): Stringer · damaged · Jan 5, 2023 · N14106 · Boeing 757224 · Fuselage Main, Longeron/Stringer
  > UPON DAMAGE REMOVAL OF FUSELAGE SKIN SECTION REF. L/P: 3443028, BETWEEN STA. 620 - 640, STRINGER S9L ALSO FOUND DAMAGED COMPLIED WITH INSPECTION REQUIREMENTS FOR VERIFICATION OF MAT''L FOR HAT SECTION DOUBLER AND FILLER MAT''L PER SRM: 53-00-03-2R-1 STEP 3. CU
- [SDR CALA2023010600046](https://openairdocs.org/sdr/CALA2023010600046.md): Skin · dented · Jan 5, 2023 · N14106 · Boeing 757224 · Fuselage Main, Plate/Skin
  > DURING JETBRIDGE CONNECTION TO THE AIRCRAFT THE JETBRIGDE CONTACTED THE AIRCRAFT FUSELAGE FWD OF D2L. INSPECTED DENT REF SRM 53-00-01 SHEET 3 PARA B,F,I,J.. DENT IS OUT OF LIMITS BUT MEETS ALL CRITERIA LISTED IN PARAGRAPH "I". APPROVED FOR DIP PER THIS SRM WI
- [SDR CALA2023010200011](https://openairdocs.org/sdr/CALA2023010200011.md): Skin · handler error · Jan 2, 2023 · N14106 · Boeing 757200 · Standard Practices/Structures
  > DURING JETBRIDGE CONNECTION TO THE AIRCRAFT THE JETBRIGDE CONTACTED THE AIRCRAFT FUSELAGE FWD OF D2L. INSPECTED DENT REF SRM 53-00-01 SHEET 3 PARA B,F,I,J.. DENT IS OUT OF LIMITS BUT MEETS ALL CRITERIA LISTED IN PARAGRAPH "I". APPROVED FOR DIP PER THIS SRM WI
- [SDR CALA2023010200010](https://openairdocs.org/sdr/CALA2023010200010.md): Toilet · leaking · Jan 2, 2023 · N14106 · Boeing 757224 · Waste Disposal System
  > RIGHT AFT LAV LEAKING BLUE WATER.CARPETS SOAKED RH AFT LAV LEAK INSPECTED. NO ISSUES NOTED.
- [SDR CALA2022123003525](https://openairdocs.org/sdr/CALA2022123003525.md): Anti-Ice Valve · faulted · Dec 30, 2022 · N14106 · Boeing 757224 · Engine Anti-Icing System
  > RTO AT 90KTS FOR R ENG ANTI-ICE CAUTION RETURNED TO GATE. REMOVED & REPLACED PRESS REGULATOR ANTI-ICE SHUTOFF VALVE. OPS CHK GOOD.
- [SDR CALA2022081902121](https://openairdocs.org/sdr/CALA2022081902121.md): Floorbeam · corroded · Aug 17, 2022 · N14106 · Boeing 757200 · Fuselage Main, Floor Beam
  > SUPPORT TASK: MAIN CABIN FLOORBEAM STA 720 RBL24 UPPER SURFACE CORRODED. TRANSCRIBED FROM HAECO GSO NRC# 9282606 REMOVED CORROSION ON FLOORBEAM AT STA 720 PER B757-200 SRM 51-1 HAECO GSO MECH V934114 INSP QC470 0-02. ORIGINAL MATERIAL THICKNESS.125, MATERIAL
- [SDR CALA2022081602103](https://openairdocs.org/sdr/CALA2022081602103.md): Doubler · none · Aug 15, 2022 · N14106 · Boeing 757200 · Horizontal Stabilizer, Plate/Skin
  > (SUPPORT TASK) RIGHT HORIZONTAL STAB INSPECTED PER EA 5100-02345 -017, FOUND 1EA REPAIR DOUBLER APPROX WIDTH=5", LENGTH= 10.5" BE TWEEN RIB 8 AND RIB 9, LOWER SKIN AUX AND FRONT SPAR. SKIN DOUBLER IS IN GOOD CONDITION. NO HISTORY OF DOCUMENTATION. TRANSCRIB E
- [SDR CALA2022081602102](https://openairdocs.org/sdr/CALA2022081602102.md): Lamp · inoperative · Aug 15, 2022 · N14106 · Boeing 757200 · Doors
  > (SUPPORT TASK) L1 DOOR EXTERIOR SLIDE LIGHT INOP. TRANSCRIBED GF FROM HAECO NR 9283359.
- [SDR CALA2022081002031](https://openairdocs.org/sdr/CALA2022081002031.md): Skin · none · Aug 9, 2022 · N14106 · Boeing 757224 · Passenger/Crew Doors
  > (SUPPORT TASK) R1 DOOR INSPECTED PER EA-5100-02345-017, FOUND 1E A SKIN DOUBLER APPROX WIDTH=8" X HEIGHT=9". SKIN DOUBLER IS IN GOOD CONDITION WITH NO DEFECTS NOTED. TRANSCRIBED FROM HAECO GSO NRC# 9282054 LOW FREQUENCY EDDY CURRENT (LFEC) INTERVAL 3,000 DOOR
- [SDR CALA2022080501958](https://openairdocs.org/sdr/CALA2022080501958.md): Seat Track · corroded · Aug 3, 2022 · N14106 · Boeing 757224 · Fuselage Main, Structure
  > SUPPORT TASK: MAIN CABIN STA 745 RBL45 SEAT TRACK SUPPORT UPPER FLANGE HAS CORROSION. TRANSCRIBED FROM HAECO GSO NRC# 9282392
- [SDR CALA2022080501957](https://openairdocs.org/sdr/CALA2022080501957.md): Attach Angle · cracked · Aug 3, 2022 · N14106 · Boeing 757224 · Wing, Attach Fittings
  > SUPPORT TASK: LW ADAPTER PLUG HAS A CRACKED ANGLE. TRANSCRIBED FROM HAECO GSO NRC# 9282883 REPAIRED LW ADAPTER PLUG UPPER ATTACH ANGLE PER UAL EC/RA 5730-0 3543. HAECO GSO MECH V900579, INSP QC004
- [SDR CALA2022080101925](https://openairdocs.org/sdr/CALA2022080101925.md): Floor Support · corroded · Jul 31, 2022 · N14106 · Boeing 757200 · Fuselage Main, Floor Beam
  > SUPPORT TASK: 1602. MAIN CABIN FLOOR SUPPORT FRAME HAS CORROSION TOP & BOTTOM. MARKED IN RED). DOT B871. STA 740 OR APPROX LBL 56. TRANSCRIBED FROM HAECO GSO NR 9282532
- [SDR CALA2022072901916](https://openairdocs.org/sdr/CALA2022072901916.md): Frame · gouged · Jul 27, 2022 · N14106 · Boeing 757224 · Fuselage Main, Frame
  > THE REPAIR INCORPORATED VIA ECRA 5362-01038 AT STA 1640 S-5R TO S-6R IS APPROVED AS TIME LIMITED FOR 18 MONTHS PENDING THE RESUL TS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE ACFT FROM SE RVICE ON JANUARY 15,2024 UNLESS ANOTHER 8110-3 FORM IS RECEIVED FI
- [SDR CALA2022072701892](https://openairdocs.org/sdr/CALA2022072701892.md): Flange · gouged · Jul 27, 2022 · N14106 · Boeing 757200 · Fuselage Main, Frame
  > THE REPAIR INCORPORATED VIA ECRA 5362-01038 AT STA 1640 S-5R TO S-6R IS APPROVED AS TIME LIMITED FOR 18 MONTHS PENDING THE RESUL TS OF A DAMAGE TOLERANCE ANALYSIS (DTA). REMOVE THE ACFT FROM SE RVICE ON JANUARY 15,2024 UNLESS ANOTHER 8110-3 FORM IS RECEIVED FI
- [SDR CALA2022072501864](https://openairdocs.org/sdr/CALA2022072501864.md): Intercostal · none · Jul 22, 2022 · N14106 · Boeing 757 · Fuselage Miscellaneous Structure
  > (B757-53-3-0492) FWD PIT RH SIDE INTERCOSTAL HAS 1EA ELONGATED HOLE AT APPROX STA 725 BETWEEN S27R AND S28R. STREAMER ATTACHED. TRANSCRIBED FROM HAECO GSO NR 9282942 MAT''L ID 7075-0.032 PO NO. 857 IAW BAC DWG 143N5375 REV C, FORM 51-21-10. INSTALLED INTECOST
- [SDR CALA2022072001825](https://openairdocs.org/sdr/CALA2022072001825.md): Frame · damaged · Jul 19, 2022 · N14106 · Boeing 757200 · Fuselage Main, Frame
  > (B757-53-3-05770 FRAME STA. 1220RH - STR.1 - TOOLING MARK/DAMAGE/BARE METAL EXPOSED ON EXTERNAL SRUFACE OF FRAME HAECO GSO NR 9283098 MAT ID 7075.0.080 IAW B757-200 SRM 53-00-07-1A-1, FORMED AND HE AT TREATED IAW BAC5602 REV A. LOCATED/DRILLED IAW B757-200 SR
- [SDR CALA2022071801780](https://openairdocs.org/sdr/CALA2022071801780.md): Intercostal · corroded · Jul 15, 2022 · N14106 · Boeing 757224 · Fuselage Main, Structure
  > B757-53-3-0553: INTERCOSTAL UPPER SURFACE CORRODED AT RBL45 BS 3 25, TRANSCRIBED FROM HAECO GSO NRC# 9283132
- [SDR CALA2022071501751](https://openairdocs.org/sdr/CALA2022071501751.md): Floor Support · corroded · Jul 14, 2022 · N14106 · Boeing 757200 · Fuselage Miscellaneous Structure
  > SUPPORT TASK MAIN CABIN STA 345-365 LBL 65 GUTTER SUPPORT HAS CO RROSION ON UPPER SURFACE, TRANSCRIBED FROM HAECO GSO NR 9283207
- [SDR CALA2022071501739](https://openairdocs.org/sdr/CALA2022071501739.md): Intercostal · corroded · Jul 13, 2022 · N14106 · Boeing 757200 · Fuselage Main, Structure
  > SUPPORT TASK: MAIN CABIN STA 399 RBL 45-61 FLOOR SUPPORT INTERCOSTAL HAS CORROSION ON BOTTOM. TRANSCRIBED FROM HAECO GSO NRC# 9 283237 REMOVED AND REPLACED FLOOR SUPPORT FROM STA 399 RBL-45 TO 61 IAW B757-200 SRM 51-40-02, SRM 51-40-05 AND BAC DWG 141N5162.
- [SDR CALA2022071501738](https://openairdocs.org/sdr/CALA2022071501738.md): Stringer · elongated · Jul 13, 2022 · N14106 · Boeing 757200 · Fuselage Main, Structure
  > SUPPORT TASK; MAIN CABIN STATION 1560-STR-16 R HAS AN ELONGATED FASTENER HOLE AT STRINGER CLIP ATTACH POINT TRANSCRIBED FROM HAECO GSO NR 9283268 B757 200 SRM 51 20 01 TOP COATED IAW B757 200 AMM 51 21 15 INSTALLED STRINGER REPAIR FR 1560 S16 R, ZONE 1 TYPE 1

Next page: https://openairdocs.org/aircraft/N14106/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 = 'N14106' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N14106/reports

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